FLIGHT TRANSPORTATION LABORATORY REPORT R94-5 DEPARMN ANALYSIS OF AIRCRAFT SURFACE MOTION AT BOSTON LOGAN INTERNATIONAL AIRPORT A OF Robert Elias Alhanatis Cab September 1994 ig, M ass 23 =MNW11 1111011,11111, ACHVEs ANALYSIS OF AIRCRAFT SURFACE MOTION AT BOSTON LOGAN INTERNATIONAL AIRPORT by Robert Elias Alhanatis B.S. Aerospace Engineering Boston University, 1992 Submitted to the Department of Aeronautics and Astronautics in Partial Fulfillment of the Requirements for the Degree of MASTER OF SCIENCE at the Massachusetts Institute of Technology September 1994 © 1994 Robert Elias Alchanatis All Rights Reserved The author hereby grants to MIT permission to reproduce and to distribute publicly paper and electronic copies of this thesis document in whole or in part. Signature of the Author..................................................................................... Department of Aeronautics and Astronautics July 13, 1994 Certified by..............................................................................................--. Professor Robert W. Simpson Director, Flight Transportation Laboratory Thesis Supervisor ... .-A ccepted by.......................................................................................... Professor Harold Y. Wachman Chairman, Department Graduate Committee ..... -. E s-.. ----.-3.% -- *"7-'-r'-7--'..,-T'^-" C - -9---'r-1--.r.w:s::--.---:.--..,s.l ..-. t- M= M1111WIdii, ANALYSIS OF AIRCRAFT SURFACE MOTION AT BOSTON LOGAN INTERNATIONAL AIRPORT by ROBERT ELIAS ALHANATIS Submitted to the Department of Aeronautics and Astronautics in Partial Fulfillment of the Requirements for the Degree of Master of Science in Aeronautics and Astronautics ABSTRACT The purpose of this thesis is to examine the nature of aircraft surface motion on the airport surface during normal operations. Twelve hours of radar data, gathered by MIT Lincoln Laboratories from Logan airport in Boston, were made available for this study. Specifically, the data included target position reports from the ASDE-3 surface surveillance radar and the ASR-9 radar from the near terminal airspace information. This data covers a variety of runway configurations, weather conditions, traffic levels and high or low visibility conditions. The study is divided into three sections. The first one focuses on the runway, and examines occupancy times, exit velocities, exit usage and velocity profiles of the final approach and landing phase. The second section, analyzes fourteen runway-taxiway intersections. Results are presented for the crossing times and usage of these intersections. The analysis also focuses on relating crossing times and usage to crossing direction, runway configuration and aircraft size. Finally, average taxiway velocities and the overall taxiway usage is measured. Additionally, the role that the location of the taxiway segment as well as its length, plays in the variation of these velocities are examined. Where possible, this study includes means, standard deviations and sample sizes of the variables in question. Thesis Supervisor: Dr. Robert W. Simpson Director, Flight Transportation Laboratory 11IN1110111IM111w, Acknowledgments I would like to thank several people for their time and support throughout the process of writing this thesis. First of all, I would like to extend my sincere gratitude to Professor Robert Simpson, my thesis supervisor, for his constant support and guidance. I am truly grateful for the opportunity to have worked with him. I would also like to thank MIT Lincoln Labs for providing the data for this thesis Jerry Welch, Ted Morin and Jim Eggert for assisting me in getting the particular in and data, answering my questions and providing me with many useful suggestions. Additionally, I would like to thank John Pararas, Dennis Mathaisel and Husni Idris for their help in developing the data processing software and the GMS interface. I would also like to thank Professor Amadeo Odoni for his insightful remarks and Professor Peter Belobaba for teaching the Airline Management and Airline Econimics courses during my studies. I would also like to express my thanks to all my fellow classmates. My stay at the Flight Transportation Lab has been a rewarding experience thanks to them. Finally, and most importantly, I would like to express my deepest gratitude to my parents for their continues love and support. R. A. Cambridge, Massachusetts July, 1994 11=1191, "Jilik 1, , '' I101,111111111M Table of Contents A bstract.................................................................................................................... A cknow ledgm ents.................................................................................................... ...... .... .. Table of Contents................................................................................ List of Tables.......................................................................................................--. .. List of Figures.................................................................................................... 3 5 7 9 10 Chapter 1: Introduction..................................................................................... Background........................................................................ 1.1 M otivation........................................................................ 1.2 Scope.................................................................................. 1.3 14 14 16 16 Chapter 2: The M easurement Task................................................................. 18 2.1 2.2 2.3 2.4 Chapter 3: D ata A nalysis................................................................................ 3.1 3.2 3.3 3.4 3.5 3.6 Chapter 4: Introduction........................................................................ The Runway and Taxiway System..................................... D ata Collection................................................................. Available D ata................................................................... Introduction........................................................................ Preliminary D ata Processing............................................. Data Irregularities.............................................................. Runway A nalysis ............................................................. 3.4.1 Runway Occupancy Time During Landing........... 3.4.2 Exit U se................................................................. 3.4.3 Exit Velocities............................ 3.4.4 Velocity Profiles.................................................... Landing Velocity Profiles.............. 3.4.4.1 Final Approach Velocity Profiles..... 3.4.4.2 Intersection A nalysis ........................................................ 3.5.1 Intersection Crossing Tim es................................... 3.5.2 Intersection U se........................................................ Taxiway A nalysis................................................................. 3.6.1 Taxiw ay A verage Velocity....................................... 3.6.2 Taxiw ay U se............................................................. Conclusions...................................................................................... 4.1 4.2 4.3 4.4 4.5 Introduction.......................................................................... Runways............................................................................... Intersections.......................................................................... Taxiways.............................................................................. Directions for Future Research............................................. References................................................................ . ................... 18 19 24 25 29 29 30 35 36 36 50 58 70 70 83 90 90 103 106 106 110 121 121 122 123 124 124 126 1111116111111111 ill, List of Tables Chapter 2 2.2 The Runway and Taxiway System Table 2.2 Runway Configurations at Logan Airport......................... 2.4 Available Data Runway Configuration for Data Block-1............................. Table 2.4.1 Weather information for Data Block-I................................ Table 2.4.2 Table 2.4.3 Runway Configuration for Data Block-2............................. Table 2.4.4 Weather information for Data Block-2................................ Runway Configuration for Data Block-3............................. Table 2.4.5 Weather information for Data Block-3................................ Table 2.4.6 Runway Configuration for Data Block-4............................. Table 2.4.7 Table 2.4.8 Weather information for Data Block-4................................ Table 2.4.9 Runway Configuration for Data Block-5............................. Weather information for Data Block-5................................ Table 2.4.10 Table 2.4.11 Runway Configuration for Data Block-6............................. Table 2.4.12 Weather information for Data Block-6................................ Runway Configuration for Data Block-7............................. Table 2.4.13 Table 2.4.14 Weather information for Data Block-7................................ Runway Configuration for Data Block-8............................. Table 2.4.15 Table 2.4.16 Weather information for Data Block-8................................ Table 2.4.17 Runway Configuration for Data Block-9............................. Table 2.4.18 Weather information for Data Block-9................................ Runway Configuration for Data Block-10........................... Table 2.4.19 Table 2.4.20 Weather information for Data Block-10.............................. 21 Chapter 3 3.2 Prelimin ary Data Processing Table 3.2.1 Typical Sample Information about a Target...................... Series of Nodes that Define the Airport Run. & Tax........ Table 3.2.2 3.4.1 Runway Occupancy Time During Landing Table 3.4.1.1 : Average Occupancy Time During Landing...................... Table 3.4.1.2 : Exits Links Runways 27, 9............................................... Table 3.4.1.3 : Exits Links Runways 33L, 15 R....................................... Table 3.4.1.4 : Exits Links Runways 4L, 22R........................ Exits Links Runways 4R, 22L.......................................... Table 3.4.1.5 : 3.4.2 Exit Use Classification of Aircraft.................................................... Table 3.4.2 3.5.1 Intersection Crossing Times Series of Links that Corresponds to Each Intersection......... Table 3.5.1 3.5.2 Intersection Use Number of Aircraft Using Each Intersection...................... Table 3.5.2 30 32 36 37 37 40 40 50 92 103 List of Figures Chapter 2 2.2 The Runway and Taxiway System Figure 2.2.1 Boston Logan International Airport - Location Map......... 19 Figure 2.2.2 : Runway and Taxiway Configuration - Logan Airport....... 20 Figure 2.2.3 : Taxiway System Around the Terminal Area.................... 23 Chapter 3 3.2 Preliminary Data Processing Figure 3.2.1 : Logan Airport - GMS Format.............................................. Figure 3.2.2 : N ode-Link Network............................................................. 3.4 Runway Analysis 3.4.1 Runway Occupancy Time During Landing Figure 3.4.1.1 : Runw ay 33L/15R................................................................. Figure 3.4.1.2 : Runw ay 27/9......................................................................... Figure 3.4.1.3 : Runways 4R/22L, 4L/22R and 15L/33R.............................. Figure 3.4.1.4 : Aver. Occup. Time During Landing Run 4R Block 1........ Figure 3.4.1.5 : Run 4R Block 6........ Figure 3.4.1.6 : Run 4R Block 9........ Figure 3.4.1.7 : Run 22L Block 8...... Figure 3.4.1.8 : Run 22L Block 10.... Figure 3.4.1.9 : Run 27 Block 2......... Figure Figure Figure Figure Figure Figure Figure 3.4.1.10: 3.4.1.11: 3.4.1.12: 3.4.1.13: 3.4.1.14: 3.4.1.15: 3.4.1.16: 3.4.2 Exit Use Figure 3.4.2.1 : Exit Use per Aircraft Class Figure 3.4.2.2 : Exit Use per Aircraft Class Figure 3.4.2.3 : Exit Use All Classes Figure 3.4.2.4 : Exit Use All Classes Figure 3.4.2.5 : Exit Use per Aircraft Class Figure 3.4.2.6 : Exit Use per Aircraft Class Figure 3.4.2.7 : Exit Use All Classes Figure 2.4.2.8 : Exit Use All Classes Figure 3.4.2.9 : Exit Use per Aircraft Class Figure 3.4.2. 10: Exit Use per Aircraft Class Figure 3.4.2.11: Exit Use per Aircraft Class Figure 3.4.2.12: Exit Use per Aircraft Class Figure 3.4.2.13: Exit Use per Aircraft Class Run 27 Block 3......... Run 27 Block 8......... Run 27 Block 10....... Run 33L Block 2...... 33 34 38 39 41 43 43 44 45 45 46 46 47 47 48 48 Run 33L Block 5...... Run 15R Block 4...... 49 Run 15R Block 7...... 49 Run Run Run Run Run Run Run Run Run Run Run Run Run 4R Block 1........ 4R Block 6........ 4R Block 9........ 22L Block 8...... 22L Block 10.... 27 Block 2......... 27 Block 3......... 27 Block 8......... 27 Block 10....... 33L Block 2...... 33L Block 5...... 15R Block 4...... 15R Block 7...... 51 51 52 53 53 54 54 55 55 56 56 57 57 Nlbhw I 3.4.3 Exit Velocities Run 4R Block 1........ Average Exit Vel All Classes Run 4R Block 6........ Figure 3.4.3.2 : Run 4R Block 9........ Figure 3.4.3.3 : Run 22L Block 8...... Figure 3.4.3.4 : Run 22L Block 10.... Figure 3.4.3.5 : Run 27 Block 2......... Figure 3.4.3.6 : Run 27 Block 3......... Figure 3.4.3.7 : Run 27 Block 8......... Figure 3.4.3.8 : Run 27 Block 10....... Figure 3.4.3.9 : Run 33L Block 2...... Figure 3.4.3.10: Run 33L Block 5...... Figure 3.4.3.11: Run 15R Block 4...... Figure 3.4.3.12: Run 15R Block 7...... Figure 3.4.3.13: Average Exit Vel per Aircraft Class Run 4R Block 1........ Figure 3.4.3.14: Run 4R Block 6........ Figure 3.4.3.15: Run 22L Block 10.... Figure 3.4.3.16: Run 27 Block 2......... Figure 3.4.3.17: Run 27 Block 10....... Figure 3.4.3.18: Run 33L Block 2...... Figure 3.4.3.19: Run 33L Block 5...... Figure 3.4.3.20: Run 15R Block 4...... Figure 3.4.3.21: Run 15R Block 7...... Figure 3.4.3.22: 3.4.4 Velocity Profiles Landing Velocity Profiles 3.4.4.1 Run 4R Block 1........ Landing Velocity Profiles Figure 3.4.4.1.1: Run 4R Block 6........ Figure 3.4.4.1.2: Run 4R Block 9........ Figure 3.4.4.1.3: Run 22L Block 8...... Figure 3.4.4.1.4: Run 22L Block 10.... Figure 3.4.4.1.5: Run 27 Block 2......... 3.4.4.1.6: Figure Run 27 Block 3......... Figure 3.4.4.1.7: Run 27 Block 8......... Figure 3.4.4.1.8: Run 27 Block 10....... Figure 3.4.4.1.9: Run 33L Block 2...... Figure 3.4.4.1.10: Run 33L Block 5...... Figure 3.4.4.1.11: Run 15R Block 4...... Figure 3.4.4.1.12: Run 15R Block 7...... Figure 3.4.4.1.13: Profiles Velocity Approach Final 3.4.4.2 Run 4R Block 1........ Final Approach Velocity Profiles Figure 3.4.4.2.1: Run 4R Block 6........ Figure 3.4.4.2.2: 4R Block 9........ Run Figure 3.4.4.2.3: 22L Block 8...... Run Figure 3.4.4.2.4: 22L Block 10.... Run Figure 3.4.4.2.5: 27 Block 2........ Run 3.4.4.2.6: Figure Run 27 Block 3......... Figure 3.4.4.2.7: 27 Block 8......... Run Figure 3.4.4.2.8: 27 Block 10....... Run Figure 3.4.4.2.9: Run 33L Block 2...... Figure 3.4.4.2.10: 33L Block 5...... Run Figure 3.4.4.2.11: 15R Block 4...... Run Figure 3.4.4.2.12: Run 15R Block 7...... Figure 3.4.4.2.13: Figure 3.4.3.1 : 3.5 Intersection Analysis 58 59 59 60 60 61 61 62 62 63 63 64 64 65 66 66 67 67 68 68 69 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 84 85 85 86 86 87 87 88 88 89 89 3.5.1 Intersection Crossing Times Figure 3.5.1.1 : Typical Intersection.............................................................. Figure 3.5.1.2 : Logan's Intersections........................................................... Figure 3.5.1.3 : Average Intersection Crossing Times Block 1......... Figure. 3.5.1.4 : Block 2......... Figure 3.5.1.5 : Block 3. Figure 3.5.1.6 : Block 4. Figure. 3.5.1.7 : Block 5. Figure 3.5.1.8 : Block 6. Figure 3.5.1.9 : Block 7. Figure 3.5.1.10: Block 8......... Figure: 3.5.1.11: Block 9......... Figure: 3.5.1.12: Block 10....... Figure 3.5.1.13: Avg. Inters. Cros. T.In Dir Int. 10, 11, 12, 13, 14...... Figure 3.5.1.14: Avg. Inters. Cros. T. Out Dir Int. 10, 11, 12, 13, 14...... Figure 3.5.1.15: Avg. Inters. Cros. T. Int Dir Int. 6................................ Figure 3.5.1.16: Avg. Inters. Cros. T. Out Dir Int. 6................................ Figure 3.5.1.17: Figurei 3.5.1.18: Figure 3.5.1.19: Figure 3.5.1.20: 3.5.2 Figure Figure Figure Figure 3.6 Avg. Int.. Avg. Int.. Avg. Int.. Avg. Int.. Cros. T. per Aircraft Class Cros. T. per Aircraft Class Cros. T. per Aircraft Class Cros. T. per Aircraft Class Intersection Use Number of Aircraft Using Each Intersection 3.5.2.1 : Configuration : Arr : 4R, 4L 3.5.2.2 : Configuration : Arr: 33L 3.5.2.3 : Configuration : Arr: 27, 22L 3.5.2.4 : Configuration : Arr: 15R Taxiway Analysis 3.6.1 Block 1.................... Block 2.................... Block 4.................... Block 5.................... Dep Dep Dep Dep 94 94 95 95 96 96 97 97 98 98 99 99 100 100 101 101 102 102 : 9, 4L................ 104 : 33L, 22R......... 104 : 22R, 22L......... 105 : 9, 15R.............. 105 Taxiway Average Velocity Figure 3.6.1.1 : Average Velocity in Taxiways............................................. Figure 3.6.1.2 : Average Velocity in Taxiways Various Lengths....... Figure 3.6.1.3 : Average Velocity in Taxiways Various Locations..... Figure 3.6.1.4 : Average Velocity in Taxiways Various Loc.&Leng.. 3.6.2 Taxiway Use Figure 3.6.2.1 : Taxiway use Inner and Outer Taxilane Block 1......... Figure 3.6.2.2 : Block 2......... Figure 3.6.2.3 : Block 3......... Figure 3.6.2.4 : Block 4......... Figure 3.6.2.5 : Block 5......... Figure 3.6.2.6 : Block 6......... Figure 3.6.2.7 : Block 7......... Figure 3.6.2.8 : Block 8......... Figure 3.6.2.9 : Block 9......... Figure 3.6.2.10: Block 10....... Figure 3.6.2.11: Taxiway use Supporting Taxiways Block 1......... Figure 3.6.2.12: Block 2......... Figure 3.6.2.13: Block 3......... Figure 3.6.2.14: Block 4......... Figure 3.6.2.15: Block 5......... Figure 3.6.2.16: Figure 3.6.2.17: Figure 3.6.2.18: Figure 3.6.2.19: Figure 3.6.2.20: 90 91 Block 6......... Block 7......... Block 8......... Block 9......... Block 10....... 107 108 109 109 111 111 112 112 113 113 114 114 115 115 116 116 117 117 118 118 119 119 120 120 iih Chapter 1 Introduction 1.1 Background After forty years of regulation by the Civil Aeronautics Board, in 1978 Congress enacted the Airline Deregulation Act, which phased out economic regulation of the industry. In the years following deregulation many new carriers entered the airline industry. The old and the new airlines soon started servicing new city-pair markets, offering expanded services and competitive fares. These developments resulted in a significant increase in the overall traffic levels. In order to provide higher schedule frequencies and more efficient use of their fleet, the airlines soon abandoned the point-to-point route networks and adopted hub and spoke network systems that concentrated traffic around hub airports. U11111fil., , M il1116 1 The increased passenger traffic coupled with the concentration of this traffic around, led to congestion within the available airspace and subsequent delays in these hub airports. Due to the aforementioned reasons, the need to develop means for greater efficiencies in aircraft operations became apparent. Major efforts are undertaken today, focusing on the use of advanced technologies for airborne and ground traffic control systems in a concentrated effort to decrease the unused airspace and increase airport capacity while simultaneously maintaining or even increasing safety levels. One such area of focus is the airport surface, where especially in periods of low visibility, aircraft experience significant delays on their way to the gate or departing runway. During the last decade, various systems have been conceptualized and are currently under development which deal with problems controllers and pilots face every day on the airport surface. The major objective of these surface traffic systems is to enhance the safety, capacity, and productivity of these airports, while at the same time reducing delays and the workload of both controller and pilot. This is accomplished via the development of advanced communications, surveillance and automation techniques for use in the control towers of major airports. Various subsystems address isolated problems such as runway incursions, taxiway guidance and surface traffic surveillance. Airport safety is intrinsically linked to capacity. The spacing between aircraft necessarily reduces with increasing capacity, and safety suffers unless the reduction in spacing is done carefully. The suggested long term solution is a surface traffic management system that will address all these subsets of problems in an integrated manner and safely control the airport surface area. Such a system must address the capacity issues of ground congestion and effective departure sequencing through the implementation of efficient routing and sequencing of aircraft on the surface, thereby the system would decrease delays and increase airport safety. In order for such a system to be successfully developed and implemented, information about the nature of aircraft motion on the airport surface must be detailed. 1.2 Motivation Few studies have been conducted to date on aircraft motion on the airport surface during normal operations. In 1960 the Airborne Instruments Laboratory at Cornell University published a series of reports about velocities and accelerations of aircraft at Kennedy Airport in New York. Later, in 1972 the Flight Transportation Laboratory at MIT studied the air-side activity of Boston Logan and Atlanta airports. Measurements were taken for runway occupancy times, velocity profiles along the runways, taxiway speeds and intersection delays. Unfortunately, most of the aircraft that operated during those years are not in service today. Additionally, the data was gathered solely in periods of good visibility and therefore the data of these reports is of little value today. It is therefore of vital interest to measure the surface movements of today's aircraft as completely and effectively as possible. 1.3 Scope An aircraft engages in a series of non-uniform and complex maneuvers on its way to the gate or the departing runway. A departing aircraft for example, after getting the clearance to push back from the gate, has to follow a taxi route that will lead it to the takeoff runway. This path varies depending on the layout of the taxiway system, the Owwo current runway configuration, and the location of the gate. It might be short or long and might involve a considerable number of turns, stops, taxiway and runway crossings, and varying length segments of straight taxing. Along this route, the pilot must be constantly be aware of the position, not only of his own aircraft, but also of nearby aircraft, ground vehicles (or even terminal buildings) in order to taxi safely and avoid any collisions. The ability of the pilot to successfully taxi along the path depends on various factors. These include the type (size) of aircraft that the pilot operates, the amount of traffic at that particular instant at the airport, the surface visibility, the weather and surface conditions, and the familiarity that the pilot might have with the specific taxiway system. We must remember also, that the pilot during his taxi, is usually assisted by the ground controller who directs him along his taxi route and provides him with information about surrounding obstacles. It is important to note though, that the pilot is the one who makes the final decisions and may override the controllers directions. For example, a controller's request for a landing aircraft to use the first available exit can be ignored, or the pilot may insist on taxiing to the starting end of a runway rather than start from an intermediate point. Such factors as the human element cannot easily be quantified and often introduce variance into the events that we want to measure, and therefore must be taken in to account in the final analysis. Among many surface motion variables that can be measured, those of interest are: the approach speed of a landing aircraft, its landing speed profile during roll-out, the runway occupancy time, the exit used, the exit velocity, the time required to cross runway intersections, and the taxiing velocities on different segments of the taxiway system. The analysis of these variables in conjunction with the major factors that affect them will be the focus of this thesis. ----N-1---'--------- - Chapter 2 The Measurement Task 2.1 Introduction The first section of this chapter describes the existing runway and taxiway system at Logan airport in Boston so the reader can get a better understanding of the airport layout and better relate the measured variables. The second section, discusses the main elements of the data collection method that was employed. Finally, the last section provides information about the different days that the data was collected. Included in this information, is a description of the weather and surface conditions as well as any particular events that occurred during the collection period and which might be of interest in the later stages of the analysis. 2.2 The Runway and Taxiway System Boston Logan International Airport lies at the edge of Boston harbor, surrounded by water in the majority of its perimeter. The commercial and residential area of East Boston is adjacent to it while the Winthrop area lies across the harbor (Figure 2.2.1). Figure 2.2.1 Logan is the dominant airport ( 70 % of the passenger traffic 1) in a regional airport system that also includes airports serving Hartford, Manchester, Worcester, Hyannis, Portland, and Providence. It has five runways with four of them (4L, 4R, 33R and 27) 1 Boston Logan International Airport Capacity Enhancement Plan, October 1992 published by the FAA. capable of handling large transport aircraft. Three of these runways (4R, 33R and 27) have instrument landing capability. The configuration of the runways is rather complex (Figure 2.2.2), as they intersect six times with each other. Figure 2.2.2 Typically, peak hour demand is 100 operations per hour. The serving capability depends on the runway operating configuration, and can vary from 46 operations per hour during the most restrictive IFR conditions to 120 operations per hour during good VFR weather 2 . This fluctuation is primarily due to the lack of parallel runways within adequate spacing between them for simultaneous IFR approaches under certain weather conditions. Consequently, at certain times all landings must be sequenced into a single arrival stream, thus lowering the airport serving capability. The high proportion of commuter aircraft operations at Logan further deteriorates the airport effective capacity, as larger separations maybe needed under certain runway configurations to safely accommodate these smaller sized aircraft due to the wake turbulence considerations during mixed (in terms of size) operations. In addition, in order to keep the noise levels that the nearby communities experience within reasonable levels, the Massachusetts Port Authority has imposed certain regulations that further complicate aircraft operations. Specifically, only certain runway configurations can be used at night and airlines are required to conduct a specific portion of their Logan operations in Stage 3 equipment 3 . The configurations 4 that are used most often at Logan are: Table 2.2 IFR VFR Configuration Arrivals Departures Arrivals Departures 1 4L & 4R 4L, 4R & 9 4R 4L, 4R & 9 2 22L & 27* 22R & 22L 22L 22R & 22L 3 33L & 33R 27 & 33L 33L 33L 15R & 9 9, 15R & 15L* 4 These configurations employ hold-short procedures. 15R 15R & 9 2,4 Boston Logan International Airport Capacity Enhancement Plan, October 1992 published by the FAA. 3 Summary of Logan's Noise Abatement Rules and Regulations published by Massport. Due to the complexity of the runway system, various procedures for intersection departures and hold-short arrival are often used. The taxiway system (Figure 2.2.3) consists of two main circumferential taxi lanes (inner & outer) around the perimeter of the terminal building area with smaller taxiway segments supporting the traffic towards the gate area. Longer taxiways also exist to feed the outbound traffic to the departure runways, and the incoming traffic to the terminal area. Runways 4R, 33L/15R and 27 have additional high speed exits conveniently located so that the landing aircraft can vacate the runway as soon as possible, and then there are various common taxi paths from these exits to the gate areas. For example, the high speed exit most commonly used for runway 4R is exit 12 (link A29-A56) , and crosses runway 4L (used only for turboprop landings and takeoffs in this case) before joining taxiway N (link A74-A75) to return to the terminal area. Zoom In) FUlIVIOW), Redraw) AO M1 Display r) ]A Edit r- Developed by the Flight Transportation Laboratory, MIT, Cambridge, Massachusetts. A7 7 Zoom Out) Zooming to full aiport view... RotatS) ut) A 5 9 2.3 Data Collection In the past, the techniques used to study the aircraft motion on the surface of airports fell into two major categories : those that involved direct observation of the traffic through a number of observers out in the airfield (the MIT study) and those involving indirect observation through the use of radar or other types of monitoring equipment. Each one of the two methods has its own advantages and disadvantages. The indirect radar method is more complex and requires expensive equipment but is fairly accurate, imposes no interference in the traffic, and once operational can be employed for long time periods. On the other hand, the other method (direct observation) is less complex but requires a large number of observers, often in coordination with each other, which involves intense manual effort and as one might suspect, and provides changing levels of accuracy. Nevertheless, both methods require the authorization and cooperation of the local FAA and airport authorities. Luckily, in our case the MIT Lincoln Laboratories had installed an experimental ground surveillance system that gathered data from Logan airport in Boston. Specifically, the data included target position reports from the ASDE-3 surface surveillance radar and the ASR-9 radar from the near terminal airspace traffic information. These two outputs of the surveillance sensors were integrated by a combined tracking system that also provided derived information about the velocity, heading and acceleration of the targets1 . A simultaneous interface with the ARTS computer was often used and then information about the aircraft type and flight number was made available. 2.4 Available Data As mentioned earlier, Lincoln Laboratory had installed a surface traffic data gathering system at Logan airport in Boston in 1993 for the development and testing of a runway status lights network (ASTA-1) to help prevent runway incursions. As much as ninety hours of traffic data were collected for this purpose. Approximately twelve of these ninety hours were preprocessed by Lincoln Labs, and made available to this study for further processing and analysis of the aircraft surface movements. These twelve hours came in the form of 10 separate blocks of data, each corresponding to an individual data gathering session. These blocks cover a variety of runway configurations, weather conditions, traffic levels, and high or low visibility conditions. A brief description of the available blocks of data follows: Block-1 Day: Thursday, April 1, 1993 Time: 16:00-17:15 Local Table 2.4.1 Runway Configuration Departures Switched to Arrivals Arrivals 4R 9, 4L 4R Table 2.4.2 Wpthpr / ATIS Temp Ceiling Departures 4R Visibility Wind 2 miles n/a 500ft ovc n/a 1800ft ovc 2 miles n/a 11 00ft ovc 2 miles Comments 50*@ 15knots Rain & Fog Rain & Fog --> Thunderstorms 40*@ 20knots Rain & Fog --> Thunderstorms 40'@24knots Block-2 Day: Friday, March 26, 1993 Time: 10:35-11:35 Local Runway Configuration Table 2.4.3 Arrivals Departures 4 9 Switched to Arrivals 33L, 27 Weather / ATIS Departures 33L, 22R Table 2.4.4 Tern Ceiling Visibility Wind 55 * F 800ft. scat 7 miles Comments 160*@7knots Heavy Traffic, All Taxiways OK. Block-3 Day: Wednesday, April 21, 1993 Time: 17:35-18:35 Local Runway Configuration Table 2.4.5 Arri Weather / ATIS Table 2.4.6 |Temp 65 * F Ceiling Visibility Wind 2500ft ovc 15miles Commients 180*@ l7knots Heavy Traffic. Block-4 Day: Tuesday, March 26, 1993 Time: 13:15-14:15 Local Run wvay Configuration Table 2.4.7 IArrivals 115R Wea. ther / ATIS em 50 *F IDepartures 19I Table 2.4.8 Ceiling Visibility Wind Sunny 12 miles 140*@7knots I Busy Traffic, later quieting down -M Comments Ph IINNIIIIIIIII Block-5 Day: Thursday, March 11, 1993 Time: 14:50-16:10 Local Runway Configuration Table 2.4.9 Arrivals 33L Departures 122R, 33L Table 2.4.10 Weather / ATIS Comments Temp Ceiling Visibility Wind 40 * F 5500ft 15 miles 300'@ l5knots Snow in the morning Block-6 Day: Wednesday, March 31, 1993 Time: 19:15-20:15 Local Table 2.4.11 Runway Configuration IArrivals DeNpartures 4R, 4L 9,4L Table 2.4.12 Weather / ATIS Temp Ceiling Visibility Wind 420 F 6500ft 15 miles Block-7 Day: Saturday, March 13, 1993 Time: 09:45-10:45 Local Runway Configuration Comments 110'@ 8knots Snow in the morning Table 2.4.13 De artures vals 9,15R Wather / ATTS Comments Temp Ceiling Visibility Wind 31 *F 5000 ft 5 miles 127' @ 8knots ILS approaches 15R 33 *F 3800 ft 12 miles 110@ l7knots ILS approaches 15R, light snow 32* F 1500ftovc 1 mile 110*@ l5knots ILS approaches 4R, light snow Day: Wednesday, April 21, 1993 Time: 19:50-20:50 Local Runway Configuration Table 2.4.15 Arrivals 22L, 27 Weather / ATIS Tern Ceiling Departures 22R, 22L Table 2.4.16 Visibilit 59 * F 2500ft scat 15 miles Wind Comments 225 *@11knots n/a Block-9 Day: Tuesday, March 30, 1993 Time: 07:45-08:45 Local Runway Configuration. Table 2.4.17 Arrivals 4 Weather / ATIS Tern Ceiling 143 * F 1700 ft Departures 9 Table 2.4.18 Visibilit |2 miles Wind Comments |40'@ l2knots Light drizzle & Fog Block-10 Day: Wednesday, April 21, 1993 Time: 09:00-10:02 Local Runway Configuration Table 2.4.19 Arrivals ep rtures 22L, 27 Weather / ATIS Tern Ceiling 60 * F 2500ftovc 22R, 27 Table 2.4.20 Visibility Wind 15 miles Comments 225@ l6knots n/a Chapter 3 Data Analysis 3.1 Introduction The first section of this chapter describes the preliminary data processing that was undertaken along with various problems that were encountered due to several data irregularities. The second section, provides a detailed runway analysis that includes information about occupancy times, exit velocities, exit use, and landing velocities profiles. The next section analyzes the intersection crossing times and the particular level of use of each intersection. Finally, an analysis of the taxiway system is presented. 3.2 Preliminary Data Processing As soon as the ten blocks of collected data were received, all the possible ways to process and analyze the available information were considered. Each block of data consisted of information about all the targets that were picked up by the ASDE-3 and ASR-9 radar during each gathering session. Every target had its own ASDE and target ID and contained among other things, position information in terms of x and y coordinates with respect to the radar location, its derived velocity, acceleration, and heading, and the corresponding time stamp for specific data items, measured in seconds from 0:00 GMT. In addition, some targets included information about the aircraft type and airline flight number (Table 3.2.1). Tt:11584 Length: 287 Start time: 5795.3 1Endtime: 58588.6 States: DEP TAX STP -deg- Target ASDE ID ID 11584 11584 11584 11584 11584 11584 11584 11584 11584 5575 5575 5575 5575 5575 5575 5575 5575 5575 Time Stamp State ASF Position (knots) 's Heading Speed Accel. ID 57995.375 57997.126 57998.878 58000.629 58002.382 58004.134 58005.885 58007.637 58009.388 1 2 3 4 5 6 7 8 9 TAX TAX TAX TAX TAX TAX TAX TAX TAX 3 North: -827.07 3 North: -827.22 g9 3 North: -802.69 3 North: -793.17 g76 North: -783.10 g76 North: -769.83 g76 North: -756.49 g76 North: -742.40 g76 North: -732.36 Flight Type Num East: 242.13 East: 249.34 East: 252.97 East: 256.41 East: 258.79 East: 263.59 East: 267.36 East: 271.39 East: 276.04 10.7 31.3 14.8 14.9 12.3 17.1 16.9 16.4 22 13.9 10.1 17.9 15.1 12.5 14 15.2 16.4 13.9 0.0874 -0.0552 0.113 0.0166 -0.042 0.0116 0.0215 0.0215 -0.0348 SR188 SR188 SR188 SR188 SR188 SR188 SR188 SR188 SR188 B747 B747 B747 B747 B747 B747 B747 B747 B747 Table 3.2.1: Typical sample information about a target inside a block of data. The individual position reports for every target, constituted a very large amount of information, and in order to be useful, had to be related again to the surface layout of the airport. A graphical replay of the information of the available data was needed since it would enable us to visualize the actual aircraft motion, check the analysis output, and explain any possible counterintuitive findings. MONOW1111110111WINA Nild HIM NOWN1111m, Recently, the Flight Transportation Laboratory at MIT had designed and developed an aircraft Ground Motion Simulator (GMS) to realistically simulate airport ground activity. The GMS simulates the environment at any arbitrary airport and provides high quality graphic views, in color on UNIX workstations. This system has an internal aircraft position generator that provides the simulation with motion updates. It was decided to use the GMS system for visualization purposes, after bypassing its position generator function and writing the necessary code to provide it with the actual aircraft motion information from the Lincoln Laboratory data. As a second step, the Logan airport geometrical layout along with its features (terminal buildings, hangars, etc.) had to be inputted in the GMS system (Figure 3.2.1). Next, the underlying network of nodes and links had to be inserted in GMS format data files in order to define the runways and taxiways of the airport (Figure 3.2.2). Table 3.2.2 lists the series of nodes that define every taxiway. The next step was to write the computer code that will associate every aircraft position with an airport link in order to be able to automate the data reduction process. Various computer subroutines were also written to perform other preliminary analyses of the recorded data. As a result, computed values were obtained for approach speeds, exit velocities, intersections crossing times, and various taxiway velocities. A more complete discussion of these values, and their significance will start in the next chapter. During the analysis process various routines had to be modified in order to overcome some irregularities in the collected data. Taxiway JIB08 A92 AV A93 B09 IA00IMA2 A42 A35 Series A36I of Nodes Y INNER OUTER z N2 1 02 D NA B 2A 01 K L N A B 00 s 101 T A55 A97 B07 A97 A56 A98 B08 A79 A29 A80 B09 A81 A99 A95 B10 BOO A96 A82 B01 B02 B03 B04 B05 B06 A83 A84 A85 A86 A70 A60 AOO A10 A20 A50 A91 A92 A93 A94 A95 A96 A80 A71 A20 A37 B04 A33 A18 A73 B06 A63 A32 B03 'A21 B14 A49 A48 A98 A79 BOO A02 A44 A04 B02 A66 A99 B05 B06 B02 B10 A72 A40 B14 A60 A32 A19 A59 A10 A64 A26 A70 A18 B13 A48 A14 A81 A77 A83 A03 A45 A05 A86 A65 A82 AOO A50 A86 B11 N2 A38 A46 A31 A01 A39 A37 A31 A25 A24 A18 A17 A16 A12 A02 A04 A07 A90 A06 A43 A44 A09 A08 A47 A48 A23 A22 A75 A74 A73 A71 A69 A66 A63 A62 A51 A52 A43 A35 B13 A34 A33 A27 A85 A53 A78 [ Runy[~~ 4R 4L 15R 22L A61 A62 A64 A65 A57 A29 A14 A45 A09 A28 A27 A26 A25 A87 4R 22R A68 A67 A72 A59 A54 A53 A42 A88 NI A39 4L 33L All A12 A13 A01 A21 A22 A78 A77 A76 15R 33R A58 A57 A55 A54 A74 A89 15L 27 A15 A06 A05 A03 A13 A17 A08 A38 B14 Ni N2 9 _B11 15L Table 3.2.2 i A23 A49 A24 A51 A47 A46 A43 A14 A52 A53 A75 A28 A36 A34 Rotate) Zoom In ZoomOut) FullView Redraw Edit r Display ) uit Zooming to full airport view.. .J 2 AGS AO 6 72 A71 9 A73 *A15 6 .5 , .15L 5 .33R 2 3 A12A11 _B.6 I baa Developed by the Flight Transportation Laboratory. MIT, Cambridge, Massachusetts. SRotate) Zoom Out) Zoom In) Full View) Redraw) Display r) Quit) Starting simulationr. - m ~-- axiing A83 30 JL...LJ1 Developed by the Flight Transportation Laboratory, MIT, Cambridge, Massachusetts. A84 3.3 Data Irregularities Due to the performance of the radar tracking system on the surface of the airport, frequently during the gathering session, an aircraft target was dropped and then picked up later on by the radar. The result was that in the data file, two different targets with separate IDs (identification numbers) could in fact have been the same aircraft, and the intermediate information about the aircraft movement between the time that the aircraft was dropped from the radar and then picked up again was not available. Another irregularity was the fact that not all targets had information about the aircraft type or flight number. This limited the classification of results according to aircraft size to only those targets where that information was available. In addition, this prevented us from identifying targets that were not aircraft but rather other ground vehicles moving on the airport surface and therefore might have infected our results if they were on the runways or taxiways. Indeed, Blocks 3, 8 and 9 did not include any information about aircraft types and flight number because the required computer tap was not in service during the collection period. 3.4 Runway Analysis 3.4.1 Runway Occupancy Time During Landing Runway occupancy time is the time over which a runway is effectively blocked (occupied) to any other traffic by a single landing or departing aircraft. As such, it potentially affects the traffic capacity of that runway. In the case when the runway is used only for landings, the runway occupancy time and its potential variations currently do not significantly affect the overall runway capacity as the inter-arrival radar separation standards of the approaching aircraft cause spacing which is almost always greater than the occupancy time. On the other hand, if the runway is used for mixed arrivals and departures, the landing occupancy time becomes more critical. In that case, the shorter the landing occupancy time, the more the time allowed to insert a takeoff between landings. This results in higher runway operational capacity, and smaller delays for the departing aircraft. Average Occupancy Time During Landing Runwa 4R 4L 22R 22L 27 9 33R_ 33L 15R 15L Data Block 1,6,9 n/a n/a 8,10 2,3,8,10 n/a n/a 2,5 4,7 n/a igure 1,2,3 n/a n/a 4,5 6,7,8,9 n/a n/a 10,11 12,13 n/a Table 3.4.1.1 The following tables (3.4.1.2 to 5) correlate each exit link of every runway from the GMS airport layout (Figure 3.4.1.1 to 3) to an exit number for the graphs that follow. Link Exit Number Runwa 27 Runwa 1 2 3 9 12 11 10 A06-A90 A05-A04 A03-A02 4 A13-AO1 5 6 7 A17-A18 A08-A09 A02-A28 A36-A15 7 6 5 A -B13 94 10 11 12 3 1 B14-A37 N1-A39 N2-A40 Table 3.4.1.2 Link Exit Number Runwal 33L Runway 15R 1 2 4 5 6 14 13 A12-A16 A13-A17 1 A01-A19 11 10 A21-A18 A22-A23 7I 8 7 96 10 11 12 5 4 1 14 2 1 Table 3.4.1.3 A14-A23 A14-A48 A52-A51 A53-A51 A53-A85 A75-A8 B11-B10 A78-A81 A77-A79 PTI Rotate) Zoom In) Zoom Out) FuIlVIew) Redraw) Display r) Edit r ) Zooming to f ull airport view... 29 by the Fgh Tsa 00 A97~ J 4 4 4 Lor 4 44 4 4 8OJ4*~ 4 4 54 N) Developed by the Flight Transportation Laboratory, MIT, Carnbridge. Massachusetts. 4 4 4 4 1 12 A 4 Rotate) Zoomin) ZoomOut) FuIlView) Redrw Displayr E g ut t Zooming out by 1.50... 8 *A 15 D l bnt Developed by the Flight Transportation Laboratory, MIT, Cambridge, Massachusetts. Exit Number I Runwa 4LRunway22RI 1 14 2 13 3 12 Link A39-N2 N1-N2 A42-A20 4 11 A43-A1O 5 6 10 9 A43-AOO A46-A60 7 8 A47-A70 8 9 7 6 A51-A86 A53-A75 10 5 A53-A85 11 4 A54-A74 12 3 A59-A73 13 2 A72-A71 14 1 A67-69 Table 3.4.1.4 Exit Number Runway 4R I Runway 22L I 2___ _ 3 4_ _ 5LJ 13 14 16 A26-A32 14 A27-A33 13 ZA3 ZI941 11 8F 12 15 2 6 10 11 A12-A16 _____16_7_7 4- 9 97 A49-A48 =7 6 iF 4 14A48 A14-A52 _2 4I- JL5-A6 3 = E Table 3.4.1.5 A57-A55 A62-A63 Rotate) Zoom in ) Zoorn Out ) Full View) Redraw) Display r Edit r) Rotating airport by 30 degrees... Devloped by the Flight Transportation Laboratory, MIT, Cambridge. Massachusetts. It The occupancy time during landing is measured from the moment the aircraft is over the runway threshold until the time it has turned in the exit and its tail has crossed the runway edge. Since our aircraft motion data was in the form of a series of discrete radar hits (approximately every 1.7 sec on the surface), the time between the first hit inside the first runway link and the first hit inside the exit link was used. In this way the size of the error was minimized. As expected before the analysis of the results, occupancy time tends to increase with the distance of the exit location from the runway threshold. This is normally true except in some cases ( Figure 3.4.1.4 Exit 12 in Runway 4R and Figure 3.4.1.7 Exit 11 in Runway 22L) where the particular angle of these exits allow aircraft to exit with higher speeds, and therefore maintain a higher average landing velocity resulting in occupancy times similar to exits that are located much closer to the threshold. Figures 3.4.1.4 through 3.4.1.16 are graphs of the average occupancy time during landing for all aircraft types over a single runway and exit for every block of collected data. It seems there exits a relationship between aircraft weight and occupancy time. We observe that usually, the standard deviation of the occupancy times are quite small (5-10 seconds) for aircraft using the first exits, unlike for those using exits that are located further down the runway. Runway 27 under configuration 2 (arrivals 27 and departures 22R) displayed the lowest occupancy time (35 seconds) for aircraft exiting at high speed from exit 6 (Figures 3.4.1.9, 10, 12). In data block 8 (Figure 3.4.1.11), with similar weather conditions but at night (20:00-21:00), most aircraft used exit number 8 (low speed) and the occupancy times were significantly larger (53 seconds). The heavier aircraft tend to land with higher velocities and require longer landing distances and therefore exit further down the runway resulting in higher occupancy times. However aircraft using a given exit have similar occupancy times, independent of aircraft size. Average Occupancy Time During Landing Block I Runway 4R Avg.Oc.Tim. Stdev. Landing Direction m q* \O knt t- W ON~ 0- C4 vE M kn\ Exit Figure 3.4.1.4 Average Occupancy Time During Landing Runway 4R Block 6 80 - Avg.Oc.Tim. - 20 70 - Stdev. - 18 N - 14 - 12 - 16 60 . 50 40 30 U -I + + -10 -6 Landing Direction 20 1 -4 -2 - eI- I IO U- I0 - N-I I V- Exit Figure 1'. 3.4.1.5 U4t 4 1- 14 .1. .4 * - - 4I~ I- Average Occupancy Time During Landing Runway 4R Block 9 Avg. Oc. Tim. 80 - Stdev. - 20 - 18 - 16 - 14 50- - 12 40 - - 10 30 - -8 10 -6 Landing Direction 20- 0 - .1e~i .nr~ .t ~t . 'I~ - .0~O :' r.ON. a U~Iu oc :/: o~ Exit Figure 3.4.1.6 44 - ~ p.e~i I~ ~ r~ . . - mr~ ~ . .4 -2 ~ ~.C -0 . - Average Occupancy Time During Landing Block 8 Runway 22L A.O.T. - 20 - 18 Stdev. - 16 --1 14 N ------- - U 12 I - 10 -8 6 Landing Direction 2 %O- i -1 e ______- If I 1.0 trn ~ e en i - Exit Figure 3.4.1.7 Average Occupancy Time During Landing Runway 22L Block 10 I IIIIIIIIIIII A .O .T -20 Stdev. - 18 - 16 U - 14 N - 12 U Landing Direction AU - 10 -8 -6 -4 -2 0 - I- I- - I - I 0 I Exit Figure 3.4.1.8 Average Occupancy Time During Landing Block 2 80 - Runway 27 Avg.Oc.Tim. - 20 -18 Stdev. - 16 70 - 60- - 14 -- 50 - - 12 40 - - 10 30 - -8 Landing Direction 20 10 0- ; - 0. - 1 2 3 4 5 I;-- I; -- ;I -- I; -- I; -= 6 7 8 9 10 11 ; - -6 -4 -2 *0 12 Exit Figure 3.4.1.9 Average Occupancy Time During Landing Block 3 80 - Runway 27 -20 .18 Avg.Oc.Tim. 70 - - 16 14 Stdev. 6050 - -- N -12 40 30 - 30 20 - -10 -8 8 Landing Direction -6 -p 10 r 1 2 3 - I - I 4 5 6 I 7 IN. i mi = a 8 Exit Figure 3.4.1.10 9 10 11 12 Average Occupancy Time During LaRng Runway 27 Block 8 80 Avg.Oc.Tim. 70 Stdev. 18 16- N 14 50 12 * 40 10 8 6 30 Landing Direction 20 2 0 *0 1 2 3 4 5 6 7 8 9 10 11 12 Exit Figure 3.4.1.11 Average Occupancy Time Durin Landin Runway 27 Block 10 S 80 - 70 - Avg.Oc.Tim. a. a U S m U IS S 50 - 40 - -20 Stdev. -18 - 16 60qJ U U -14 N -J - 2 -10 -8 Landing Direction 30 20 - -6 -4 10 - - 2 0 1 2 3 4 4. 8 U U 0 10 5 6 7 8 Exit Figure 3.4.1.12 9 10 11 12 x Aveage Occupancy Time During Landing Block 2 80 Avg.Oc.Tim. 20 70 Stdev. 18 16 N 14 60 50 - Runway 33L _ _ .-- __12 40 10 30 8 Landing Direction 4 . $ ' 6 20 4 10 * 2 M 0 14 en 10 14 'r W)j 0 1-- 00 ON 0 - en q Exit Figure 3.4.1.13 Average Occupancy Time During Landing Runway 33L Block 5 Avg.Oc.Tim. 80 2 P 20 18 Sdoccup 70 Landing Direction 16 -N 60 __ __ _ _ _ _ _ 14 _ 50 12 ' 40 10 -8 3020- 4 0 0ee Exit Figure 3.4.1.14 z ' Figure 3.4.1.15 Average Occupancy Time During Landing Runway 15R Block 7 Avg.Oc.Tim. 20 18 16 ~~-N Stdev. U U U 14 12 U U 0 41 * mE-' 8~ S Landing Direction 10 e 8 6 9 4 2 0 In eq W-4 0 ON 00 (l- %O Exit Figure 3.4.1.16 Sn 14t en q W-4 3.4.2 Exit Use Figures 3.4.2.1 through 3.4.2.13 represent graphically the exit use both for all aircraft that landed in every runway and for each aircraft (weight) class in every data block that information about the aircraft types were available. If information was available during data collection, the exit use per particular aircraft class is presented. Each aircraft is classified according to its weight into one of the following three classes: Class Weight Range ('000 LB) Heavy 300-900 Large 12.6-299 Small 0-12.5 Table 3.4.2 The major observations are that, as expected, the probability of exit is related to the aircraft size (weight class). Hence, heavier aircraft tended to use exits that are located further away from the runway threshold while smaller sized ones required shorter landing distances and exited earlier. A second factor that affected exit use was the specific turning angle of the exit. This angle (which could have been acute, right, or obtuse) provides a measure of the difficulty of using each exit. As a result, independent of runway, most aircraft tended to prefer the use of obtuse angled (high speed) exits. Exit Use per Aircraft Clases Runway 4R Block 1 37 Landings 35 Small 30 25 O Large - Heavy 20 . 15 10 Landing Direction 5 - 0 Exit - Figure 3.4.2.1 Exit Use per Aircraft Class Runway 4R Block 6 23 Landings 35 30 25 * Small 20 o Large Landing Direction * Heavy 10 5 0 V- 1 CI 2 I sr~ a ~.O a ~ -t~2 00 O~ n M 0 .Lp - e~ W-4 . en~ Exit Figure 3.4.2.2 t O W--4 Figure 3.4.2.3 Exit Us. Runway 22L Block 8 16 Landing. 40 35 30- 3AlI Classes 25 20 15 Landing Direction 10 5 t C) C i ak 00 r Wten %4V- 0 in 0 Figure 3.4.2.4 Runway 22L Block 10 16 Landings Exit Us. per Aircraft Class 40 -r a Small 35 - Large 30 t 25 Heavy 20 - 15t Landing Direction 10 I i I I VI) W-4 i qqW- i 'w-.---r--r--------- 11 P. C1 -4 W- W- 0"- ON 00 Exit Figure 3.4.2.5 11 r- i c Vr) ,iten N -4 Exit Use per Aircraft Class Runway 27 Block 2 11 Landings 100 90 Small 80 Large 70 60 Heavy 50 40 Landing Direction 30 20 10 0 1 2 3 4 5 6 7 8 9 10 11 12 10 11 12 Exit Figure 3.4.2.6 Exit Use Runway 27 Block 3 8 Landings All Classes 100 90 80 8E3All Classes 70 60 50 40 Landing Direction 30 20 10 1 2 3 4 5 6 7 Exit Figure 3.4.2.7 8 9 Exit Use Runway 27 Block 8 19 Landings All Classes 100 90 80 All Classes 70 60 50 Landing Direction 40 30 20 10 0 1 2 7 6 5 4 3 12 11 10 9 8 Exit Figure 3.4.2.8 Runway 27 Block 10 12 Landings Exit Use per Aircraft Class 60 -r 50 M Small - Large 40 Heavy 30 20 Landing Direction 10 I I 2 3 4 i 5 &- I i II ~ 4 i 7 6 Exit Figure 3.4.2.9 - 8 I II 9 i aI 10 i 11 12 Figure 3.4.2.10 Exit Use per Aicraft Class Runway 33L Block 5 37 Landings 60 ,50 - 40 E Small o Large Landing Direction 30 * Heavy 20 10 j -IW- eq I I-. I en I 14 .r-1M I I I mrn %O t- 00 Exit Figure 3.4.2.11 I. I.rm I.r1" I. 0' o W-4e'4 i I en I q Runway 15R Block 4 21 Landings Exit Use per Aircraft Class 50 45 Small 40 - 0 35 - Large 30 Heavy 25 - 20 Landing Direction 15 - i -l l 10 - 5 I. 0- I I ~ '~ I ..4i C, I I O7, 0 I I N\Q 00 1~ ':j* r 2MII I ciI Exit Figure 3.4.2.12 Exit Use per Aircraft Class Runway 1SR Block 7 28 Landings 45 40 - M Small 35 30 - 0 Large 25 - * Heavy 20 15 - Landing Direction 10 - 0 ! ! 5W-4 !IIi I ' - ci - | 0 O 00E - Eit Figure 3.4.2.13 ~.o "~ ~ ci - 3.4.3 Exit Velocities The angle of every exit plays a significant role in the exit velocity of the aircraft. As figures 3.4.3.1 through 3.4.3.13 show, whenever the landing aircraft are using the obtuse angled exits the exit velocities are significantly higher than the other ninety degrees or acute angled exits. However, this is only true for high speed exits which are accompanied with long exit segments and give the pilot room to brake (exit 6 runway 27: 38 knots and exit 5 runway 33L : 40 knots). Exit 8 of runway 4R, although it is obtuse angled, the short exit segment that follows does not allow high exit velocities. Each figure presents, using columns the average exit velocity, and with a line, one high and one low value which corresponds to the average exit velocity plus or minus one standard deviation (see figure legend). The letter H denotes a high speed exit. Average Exit Velocity All Classes Runway 4R Block 1 0 Avg. Exit Vel. O -0 50 A.E.V. + SD 40 A.E.V. - SD * 30 r 20 - Avg. Exit Vel. Landing Direction 10 0 -I MI I 14 H H W) I. r-00O > Exit Figure 3.4.3.1 N etn O Average Exit Velocity AD Classes Runway 4R Block 6 0 Avg. Ex. 60 Vel. A.E.V. + SD 50 A.E.V. - SD 40 " Avg. Ex. Vel. 30 Landing Direction 20 - 10 4. H - - - - ~ en 4 - t - W rO O 00 m . mW.L....JnL....J ii...... I ti~ - o. 0 .en ". W-4 ~* - i ir~ - \O - Exit Figure 3.4.3.2 Average Exit Velocity All Classes Runway 4R Block 9 60 0 AvgExVel 50 A.E.V. + SD 40 A.E.V. - SD 30 " AvgExVel 20 Landing Direction 10 I - - I I - ~~ C t~~1-C- 00 Os Exit Figure 3.4.3.3 0 H I~~1 - - W-4 .C4 11 W-4 W rn W-4 W- Average Exit Velocity All Classes Runway 22L Block 8 60 0 AvgExVel U, 0 50 A.E.V. + SD A.E.V. - SD 40 0 ~I. 30 ,, "AvgExVel Landing Direction 20.+ U I- 10. . v .0 . 'n .I . . . . . . . Cl4 Nt 1-4 0 ON 00 r- .in. \0 ') N eE Cxit Exit Figure 3.4.3.4 Average Exit Velocity All Classes Runway 22L Block 10 AvgExVel > 50 A.E.V. + SD 40 A.E.V. - SD 30 3 -AvgExVel Landing Direction 20 10 0 -- - -+ - -H - + -+ Exit Figure 3.4.3.5 - -+ - -- Figure 3.4.3.6 Averag JExit Velocity All Classes Runway 27 Block 3 0 60 - AvgExVel 50 . AE.V. + SD 40 A.E.V. - SD ' AvgExVel 30 20 Landing Direction 10 a '~ 1 2 3 ~ I I I 4 5 7 6 Exit Figure 3.4.3.7 8 9 10 11 12 Average Exit Velocity All Classes Runway 27 Block 8 60 O AvgExVel 50 A.E.V. + SD 40 A.E.V. - SD 30 Landing Direction " AvgExVel 20 .111. 10 U a - 0 - ------ 1 2 4 3 5 7 6 8 9 11 10 12 Exit Figure 3.4.3.8 Average Exit Velocity All Classes Runway 27 Block 10 6 AvgExVel 8 50 A.E.V. + SD 40 A.E.V. - SD - Landing Direction :* 30 AvgExVel S20 10 H 1 2 3 4 5 7 6 Exit Figure 3.4.3.9 8 9 10 11 12 a Average Exit Velocity All Classes Runway 33L Block 2 0 AvgExVel 50 A.E.V. + SD 40 A.E.V. - SD 30 , - AvgExVel S20 Landing Direction 10 -H IH 0 - 0- al Exit Figure 3.4.3.10 Average Exit Velocity All Classes Runway 33L Block 5 o AvgExVel 60 ., 50 + A.E.V. + SD A.E.V. - SD 40AvgExVel - 20 10 I W- I N~ .T1T~u I M 1W I E-rn ~1111 .10. * %O0 r- 00 Exit Figure 3.4.3.11 0*1 . o- I - IMA i - i - - Average Exit Velocity All Classes Rumway 1SR Block 4 6AvgExVel A.E.V. + SD 50 A.E.V. - SD 40 " AvgExVel 30 230 20 Landing Direction 10 H 0- 't m - 0 - 01\ 00 te' ir \0 rN + -- -- -- Exit Figure 3.4.3.12 Average Exit Velocity All Classes Ruaway 1SR Block 7 60 0 M 0 AvgExVel A.E.V. + SD 50 A.E.V. - SD 40 " AvgExVel 0 30 20 Landing Direction 'I a- 10 - 0 O~ 00 N .E~J.rb. a I \O Exit Figure 3.4.3.13 I ur) I ll 1 e 5 e4 W-4 Figures 3.4.3.14 through 3.4.3.22 show the average exit velocities per aircraft class. These velocities vary from aircraft class to aircraft class but the variation is not consistent and no conclusions can be drawn in favor of one class or another. Average Exit Velocity per Aircraft Class Runway 4R Block I * Heavy 0 Large E Small .rflI Landing Direction . --- I I -~ ~~ - ~. I' . a~'J - Exit Figure 3.4.3.14 C-4 -4 en - ~J- a - I I . Average Exit Velocity per Aircraft Class Runway 4R Block 6 50 -- 45 40 35 - H H * Heavy Landing Direction - 0 30 - 25 - Large Small 2015 10 - 50* I i I I I i i H | | 00 ExitO- | 0 I' 'II r~ -I--- - I I - - I Ir - Eit Figure 3.4.3.15 Average Exit Velocity per Aircraft Class Runway 22L BlocklO 50 Landing Direction 45 70 4035 EHeavy 30 OLarge 25 E Small H -20 15 l 10 0 Exit Figure 3.4.3.16 Ic Avenge Exit Velocity per Aircraft Class Runway 27 Block 2 50 45 40 H 35 - U Heavy ~30 0 Large : Small 25 Landing Direction 20 15 10 5 0 1 2 3 4 5 8 7 6 9 10 12 11 Exit Figure 3.4.3.17 Average Exit Velocity per Aircraft Class Runway 27 Block 10 Landing Direction 50 45 g 40 Heavy H 35 30 0 Large * Small 25 20 415 10 5 < 0 - 1 2 3 4 5 - -i -- 6 7 Exit Figure 3.4.3.18 i * 8 9 10 11 12 Average Exit Velocity per Aircraft Class Runway 33L Block 2 50 -r 45 - Landing Direction 40- * Heavy 35 - O Large 30 - 25 - Small Si 2015 10 - an 5- 0- (Nj r~ '~1* . , 0, ,N I e'q -. a e- qW-4 T Exit Figure 3.4.3.19 Average Exit Velocity per Aircraft Class Runway 33L BlockS 50 45 - * Heavy 40- U Large 35 - El Small 30 25 20Landing Direction 15 10 5 0 -* * a,1 W) 1O - 00 Exit Figure 3.4.3.20 68 o - e-i o I ~- Average Exit Velocity per Aircraft Class Runway 15R Block 4 50 - * Heavy 45 - 40 o Large - 35 - 30 E - Small 25 - 20 - Landing Direction 15 105. I I I I 0~ I en WW- (14 W1-4 0 all I r- 00 *R I '0 11t mrn eq "..4 Exit Figure 3.4.3.21 Average Exit Velocity per Aircraft Class Runway 15R Block 7 * Heavy 5045 - 40 - 0 Large O Small 35 - 30 25 - 20 - Landing Direction 15 10 - 5- 0- t I bi .Hn i1----------------i M% 00 t- Exit Figure 3.4.3.22 '. In~ 1I qt C r-J - 3.4.4 Velocity Profiles 3.4.4.1 Landing Velocity Profiles Figures 3.4.4.1.1 through 3.4.4.1.13 show the landing profiles of all aircraft that landed in each runway. The aircraft that used a particular exit are grouped together. We can observe the different exit velocities and the higher or lower deceleration that occur, depending on the angle and the location of each exit. We must note the fact that some aircraft actually speed up after the runway threshold. Figure 3.4.4.1.1 Landing Velocity Profile Runway 4R Block 6 1.2 X X 0.8 ---------------------- -- X U.X yxX o X a 0.4 ------------- X -- - - Mean Exit 8 ' Mean Exit 12 -------- 0.6 ------------------ X'-- ------------- T h r e -- 9 h - 3 Mean Exit 13 X- Mean Exit 14 0 ----------------------------0.2 d 0( e en e C'q C1 Ni 0 Ci - "I .- 1 - cc -4 Radar Hits from Run way Threshold Figure 3.4.4.1.2 Landing Velocity Profile Runway 4R Block 9 1.2 1 0.8 -' A - --------- 0.6 ------- 0.4 -X- - .. h r e ---- S - Mean Exit 7 Mean Exit 8 Mean Exit 11 -- -----.. - Mean Exit 12 0.2 ON'No C1eqC4C en 0 r- IR -q 1- 1- -1 e'i N 00 r- 0 rM 1- -4 Radar Hits from Runway Threshold Figure 3.4.4.1.3 72 OONC e C4 Landing Velocity Profile Runway 22L Block 8 Xh r Mean Exit 6 Mean Exit 8 ---- - - -- O-- Mean Exit 10 ----- Mean Exit 11 0.2 eq 0c I~ en Il 0 1%0 C4I C4i N Wc - I -. 0 %o eC4 W- C4 .C 0 qT W0 V- "- Radar Hits from Runway Threshold Figure 3.4.4.1.4 1- NO N C 0 N en Landing Velocity Profile Rmnway 22L Block 10 1.4 1.2 . 0.8 ---0.6 Mean Exit 6 -X- 0.4 Mean Exit 7 0 Mean Exit 10 -- - Mean Exit 11 0.2 R -4 M~ M 00 C4 'n C N C7i% 1%0 M - -4 - o t~- q - -4 eN i) W Wc - Radar Hits from Runway Threshold Figure 3.4.4.1.5 74 -4 q r- 0 - -4 ei mllililiih, ~ 1111, INM i IIIiliii 1,101111i Landing Velocity Profile Runway 27 Block 2 1.4 ------------------------------ ----------------------- -------------- 1.2 1 - --- 0.8 - - - - --- --- ------ ------- - m----- ------- ---------- --- ----- W------------- M-- T ------------- hr e 0.6 - ------ S 1 b 0.4 -- -- Mean Exit 6 d 0.2 -4-----------------------4------------------------------ i i i !i I I I I SiilIili eq 0% C4 -. I I I II I 11111a %O~0 I I i i i., I II I Ii e II I II II II I II II I I I II I I I II II I I mliii I I - N ii I Iloa umimi a i l uIn 1--4 00 - I iiiimmiiui I I aI "- Radar Hits from Runway Threshold Figure 3.4.4.1.6 I r- .qt 1- I 0 N mliii, g o 1 1 m C1 r4 1 Landing Velocity Profile Runway 27 Block 3 1.2 1 >0.8 -e .C 0.6 Z T h r -0 ------- 0 0.4 --- --- 0.2 o t- "qf 1- eqi ci 00 -4 in N '-4 -4- ON ~ *10 Radar Hits from Runway Threshold Figure 3.4.4.1.7 cias 00 Landing Velocity Profile Runway 27 Block 8 1.2 -r----------------------------&------------------------- 1- ---------------------------- ---- 1T . >0.8 - --------------- ----- -------- --- eO.r -ee 0.6 h - --------------- ------------ - -Mean Exit 8 0 d 0.2 --- ------------------------- --- 191 1111911 111 111 H11 0 a' N - Radar Hits from Run w'ay Threshold Figure 3.4.4.1.8 -4 00 -. 4 C4 -. 14H I C4 Landing Velocity Profile Runway 27 Block 10 1 0.8 0.6 h r e 0.4 S ------------- 0.2 Radar Hit from Runway Threshold Figure 3.4.4.1.9 Landing Velocity Profile Runway 33L Block 2 1.6 1.4 1.2 1 0.8 3 Mean Exit 5 0 Mean Exit 8 0.6 -X- a---------- b-. 0.4 Mean Exit 10 -- - Mean Exit 12 0 -q 0.2 .t -4 00 kn eq C, r- 0 % rC4 in Radar Hits from Runway Threshold Figure 3.4.4.1.10 79 t- 0 Figure 3.4.4.1.11 80 Landing Velocity Profile Runway 1SR Block 4 1 - 0.8 C *) ------------- 0.6 -- +-- Mean Exit 7 - Mean Exit 10 ----------------- 0.4 -X- 9-- Mean Exit 11 0.2 00 e. NRadar e Ca o 00 '. ".4".4". e4 o0 H - f oo e R R- ei 0 Thr c- e Radar Hits from Runway Threshold Figure 3.4.4.1.12 ' o 0 o Ce Figure 3.4.4.1.13 82 hi"I 3.4.4.2 Final Approach Velocity Profiles In the final approach velocity profile figures ( 3.4.4.2.1 through 3.4.4.2.13) we observe that in most runways, there is a small deceleration during the final approach. In some runways, 27 in particular, this deceleration is quite significant (Figure 3.4.4.2.6). In the same runway, during night operations (Figure 3.4.4.2.8) we see much more smooth final approach velocity. In runway 15 R, we note that even under different weather conditions, aircraft seem to accelerate before the runway threshold. Overall, the standard deviations of the landing velocities fall between a value of 0.2 for a period of approximately 10 radar hits before the threshold and from then on it increases significantly. This could be due to the changing size of the available number of data points (radar hits), as further away from the threshold some aircraft target are not picked up by the surface radar. Runway 4R Block 1 Final Apprch Velocity Profile 0--- 10 --- --- --- --- ----------------------------- - --- .--- 09 S0.8 ----------------------------------------------------------0.7 -------------------------- ean-----------------------------'---------------------------- 0.6 -------------- I ~0.18..0.3 -------------------------------------------------- -------- j---- 0 .2 --------------------------------------------- 0.5----------- ------------- -------------- 0 1 2 3 4 5 6 7 8 9 10 11 12 Radar Hits from Runway Threshold Figure 3.4.4.2.1 13 14 15 16 17 -maw" Final Approach Velocity Profile Runway 4R Block 6 1.2 1 1- 0.8 A 0.6 .C 0.4 0.2 0 1 2 3 4 5 6 7 8 9 10 Radar Hits from Runway Threshold Figure 3.4.4.2.2 Final Approach Velocity Profile Runway 4R Block 9 1.2 1 ~;m. 0 0.8 -0- U Mean 0.6 -- --------------.. -O-*---Stdev. 0.4 - - - ------------.....................------- -.-..----- -.- ~1 0.2 --- -- ---- - - ---- I- I-, I- 0 1 2 3 4 5 6 7 8 9 Radar Hits from Runway Threshold Figure 3.4.4.2.3 84 10 11 12 Pinal Approach Velocity Profile 1.2 S Runway 22L Block 8 ---------------------------------------------------------- -- 0.8 -. - .-- -- --- .--- - .......--- .-... S. Mean ---------------------- 0.6 ---------------------- W3 Stdev. ----------------------------------- ----------- ----------- d0.2 0 r 1 2 3 4 5 6 7 8 9 11 12 13 14 15 10 16 17 18 19 Radar Hits from Runway Threshold Figure 3.4.4.2.4 Final Approach Velocity Profile 1.2 Runway 22L Block 10 ----------------------------------------------------------- 0.8 ------------------------------------------------------0-Mean ---.....---Mean- f0.6 ------------------------ - Stdev. -3 ----------------- - 10.4 --------------------- 0.2 ---------------------------------------------------------- 0 1 2 3 4 5 6 7 8 9 10 11 12 Radar Hits from Runway Threshold Figure 3.4.4.2.5 85 13 14 15 16 Final Approach Velocity Profile Runway 27 Block 2 1.4 .------------------------------------------------------------ ------------------- 0.8 0.6 -S-----------...--- 0.4 ....... - 0.2 ---- -- -- -- -- - -=..--- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- --- .1.2 Mean - Stdev. -- ...- --..---.. ---- .. -...--.-- ..-- -- ----- - - .--- - ---- - ------- m--------------------------------------------------0~~~~3 0 1 2 4 3 5 . 6 7 8 ............ 9 10 11 i I 12 13 I 14 15 I 16 17 I 18 19 20 Radar Hits from Runway Threshold Figure 3.4.4.2.6 Final Approach Velocity Profile 1.2 Runway 27 Block 3 ---------------------------------------------------------1 --- -m- -'"''= -=--'- ===-:.3-;:=.-----.- - - - - - - - - - - - - - - - - - - - - - - - - - -- AI .------------------- ------------------------------------ S0.8 ---o---Mean 0.6 ------------------ -- -3- ----------------------- Stdev. ----------------------- e0.4 --------------m------ 0.2 .-----------------------------------------------------------0 1 2 34 5 6 7 8 9 10 11 12 13 14 Radar Hits from Runway Threshold Figure 3.4.4.2.7 86 15 16 17 18 19 Pinal Approach Velocity Profile Runway 27 Block It 1 -- - -- -------- -- -- -- -- -- -- -- ---- - - - - - - - - - - - - - 0.9 ----------------------m-----------------------------0.8 ------------- ----- --------m---------------------m----------0.7 0.6 .--------------------- N e n ---------------------0.5 ----------------- - - -- -- Stdev.-m 0.4 -------------------------------------------------------0.3 0.2 ----------------------------------------------------------------- - --- 0.1 ---------------------------Ma --- - -- --- ---.--- ----------------- -------- 0 1 2 7 8 9 10 11 12 Radar Hits from Runway Threshold Figure 3.4.4.2.8 Final Approacb Velocity Profile Runway 27 Block 10 1.2 ---------------------------------------------------------- 0.8 --------------------- --------------------- 8 0.4 - Mean -O-- Stdev. ------------------------ S0.2 ------------------ ---------------- ----------------------0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 Radar Hits from Runway Threshold Figure 3.4.4.2.9 87 18 19 20 Final Approach Velocity Profile 1.2 Runway 33L Block 2 -------------------------------..----....----...---..--..--.- 8 .--- --. I" 0.8 ------------------------------------------------------------ --- S0.6 -------------------- Mean ------------------- --- ---O--Stdev. o0.4 --------------------- .--------------- d .2 - -. --------------------------------- - -. ----... .........-- ...- 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 Radar Hits from Runway Threshold Figure 3.4.4.2.10 Final Approach Velocity Profile 1.2 . --------------------1- - -- 'c 0.8 --- Runway 33L Block 5 --.---..-..--..-....---..-------... --------------------...- - -.------.-- -- -- -- - --------- - m- -- - --- ----- 0.6 ------------ - m---.- -- --- - --....-- ..---- ...--- - .-- -Mean --- ----.---.-- .. m---...---- Stdev. e0.4 --------------------S 0.2 . -------------- -- -. - ..----... -- -- . ------------- - - ------- 0 1 2 3 4 5 6 7 8 9 10 11 12 Radar Hits from Runway Threshold Figure 3.4.4.2.11 88 13 14 15 16 17 Final Approach Velocity Profile Runway 1SR Block 4 1.4 ------------------------------------------------------------ 31 .--------------------------------------------------------- 0.8 --- ------------------------ ----------- ---------------- ------- -------------- 0.6 -- -----------------e---Mean 0.4 -- --------------- ------------------------13 Stdev. -0 ---------------0 i 2 1 3 4 ------------------------- 7 6 5 9 8 10 11 12 13 Radar Hits from Runway Threshold Figure 3.4.4.2.12 Final Approach Velocity Profile Runway 1SR Block 7 1.4 ------------------------------------------------------------ ---.. - : :... --. - - 1.2~~~~ .2 ----------------------------------------- .. =......----- --- 0.8 - --- -------------------------- ----- - 0.6 ---- ---------------------------- ---- --- D-- Mean ------ Stdev.- ------ 0.4 -- ------------------------------ ------------------------- =0.2 --- -- ------------------------------- ------------------- 0 1 2 3 4 7 6 5 8 9 Radar Hits from Runway Threshold Figure 3.4.4.2.13 89 10 11 12 13 3.5 Intersection Analysis 3.5.1 Intersection Crossing Times When an aircraft approaches an intersection it is either cleared to cross it by the ground controller, or it is instructed to stop or slow down to allow another aircraft to cross in front of it. Occasionally, in periods of heavy traffic a pilot will have to wait in a queue to cross a particular intersection or possibly wait for a queue of aircraft to pass through an intersection. Figure 3.5.1.1: Typical Intersection Due to the complexity of the runway and taxiway system at Logan airport, a departing or arriving aircraft has to cross a significant number of intersections in its way to the gate or departing runway. In order to measure the intersection crossing time as C -AA Cat accurately as possible a distance of fifty meters before and after the intersecting runway or taxiway centerline was chosen. Since the radar hits are skin returns from the center of the aircraft' s fuselage, such a distance would ensure that the calculated crossing time would include the initial crossing of the front part of the aircraft and will end after its tail has cleared the crossing runway or taxiway (Figure 3.5.1.1). The calculated crossing time was split in two segments. The first (time 1) being the time from the start until the aircraft crosses the intersecting centerline and the second segment (time 2) from the centerline until the aircraft clears the runway or taxiway. The following table lists the series of airport links corresponding to each intersection number. Intersection Series of Links 1 A16 A17 A18 2 A02 A01 A19 3 A22 A23 A48 4 A18 A24 A46 5 A08 A09 A44 6 A74 A75 A83 7 A52 A51 A86 8 A48 A47 A70 9 A24 A46 A60 10 A44 A43 A00 11 A44 A43 A10 12 A35 A43 A00 13 A35 A43 AlO 14 A35 A42 A20 Table 3.5.1 Figures 3.5.1.3 through 3.5.1.12 show the average crossing times along with the standard deviations for every intersection in the ten blocks of collected data. As figures 3.5.1.13 and 14 show there is a significant difference in average crossing time depending in the runway configuration and thus in the direction of use of some intersections. For example, when intersections 10, 11, 12, 13 and 14 are used in the inbound direction (towards the terminal area), usually after arrivals in runway 27, the crossing times seem to be much smaller compared to those of departing aircraft which use the same intersections but in the opposite direction (outbound), and often have to form a queue while waiting to depart from runway 9 and thus cross these intersections very slowly. Similarly in intersection 6 the inbound direction of crossing is much quicker (aircraft landing on runway 4R) that the outbound one (aircraft waiting to depart from 22L and 22R). Comparing the crossing times of the two different segments of each intersection (time 1 and time 2), we observe that usually when an intersection is used in the inbound direction time 2 is larger than time 1 and when it used in the outbound time 1 is larger. This could be possibly due to the fact that when a pilot is on his way to the gate, after crossing the intersection it has to slow down since the connecting taxiway segments A75-A83, A51-A86, A47-A70 etc. are short as they intersect with the circuferential outer taxi lane which is often congested. On the other hand, in the outbound direction usually time 2 is smaller than time 1 probably because the connecting taxiways that lead away from the terminal area are longer and therefore the pilot accelerates faster. Figures --- through --- show the average crossing times per aircraft class (size) for intersections where ten or more aircraft crossed them. Larger aircraft are heavier and logically should have longer crossing times but the graphs show this is the case only in few blocks of data (block 1). Block 1 Average Intersection Crossing Times 50 45 40 35 - - L-r- E3 Mean Time 1 - o Mean Time 2 - IfI 30 Stdev Time 1 25 20 * Stdev Time 2 - 15 - 10 - 5 0 L7-[L77HI~bn .... - C1 M ~' t I V) tr- ' 00 ON 0 I c~ - - - - Intersection Number Figure 3.5.1.3 Average Intersection Crossing Times Block 2 62 E) Mean Time 1 EMean Time 2 Stdev Time 1 Stdev Time 2 LFE~ I e I I ~ n n j _r.fl- A,, Lm F-J -. -" r--r---i m1--Ir~ ~ ~0 r--- 00 0~ 0 r'-r--- - e'~ - Intersection Number Figure 3.5.1.4 94 - Figure 3.5.1.5 Average Intersection Crossing Times W- eq e t n 00 M\ Intersection Number Figure 3.5.1.6 0W- Block 4 V- - C4I - en V- qt W- Average Intersection Crossing Times Block 5 50 liEl Mean Time 1 45 4035._ O Mean Time 2 E Stdev Time 25 *30. 1 --- - Stdev Time 21 20s 0 0 15 10q - M~ lq In %0 00 (ON 0 1 enI - Intersection Number Figure 3.5.1.7 Average Intersection Crossing Times 50 45 ii 40 Block 6 Mean Time 1 o- Mean Time 2 35 30 Stdev Time 1 25 20 15 10 - W-4 C14 Stdev Time 2 M It kn O t- 00 ON Intersection Number Figure 3.5.1.8 - - - - - Average Intrsection Crossing Times Block 7 50 45 40 * 35 30 25 20 15 10 5 0 q - en ' o ( 00 o 0 - e rn Intersection Number Figure 3.5.1.9 Average intersection Crossing Times Block 8 50 45 Eii mean Time 1 40 35 30 0 Mean Time 2 Eil Stdev Time 1 25 20 15 SStdev Time 2 10 5 0 T- CMJ CO e LO) Co ,. co o0 0 1v- Intersection Number Figure 3.5.1.10 1- C CO r 1 Averge Intersection Crossing Times Block 9 68 0 Mean Time 2 E Mean Time 2 Stdev Time 1 Stdev Time 2 4 nt er s0ei en 00 Nme o - - - Intersection Number Figure 3.5.1.11 Average Intersectio Crossing Times 50 45 Mean Time 1 40 DE Mean Time 2 35 30 E - Stdev Time 1 25 - 202Stdev Time 2 15 10- 0Intersct Nu m b N~~ t in r- 0-ON Intersection Number Figure 3.5.1.12 Block 10 - Average Intersection Crossing Time Inbound Direction O Block3 Tim. 1 o Block3 Tim. 2 Block8 Tim. 1 Block8 Tim. 2 BlocklO Tim. 1 BlocklO Tim. 2 '4 11 14 12 Intersection Figure 3.5.1.13 Outbound Direction Average Intersection Crossing Time O Block1 Tim. 1 Blocki Tim. 2 Block4 Tim. 1 Block4 Tim. 2 Block6 Tim. 1 O Block6 Tim. 2 E Block9 Tim. 1 10 11 12 13 Intersection Figure 3.5.1.14 14 il Block9 Tim. 2 Average Intersection Crossing Time Inbound Direction 50. 45. OiBlock1 Tim. 1 40- O Block1 Tim. 2 35 30. Block6 Tim. 1 25. Block6 Tim. 2 20. 15 Block9 Tim. 1 10. 5- 0. - -r-iA IJ Block9 Tim. 2 ................. I 6 Intersection Figure 3.5.1.15 Average Intersection Crossing Time Outbound Directic ii Block2 Tim. 1 o Block2 Tim. 2 50 , 45 - Block3 Tim. 1 40 35 . 30 - * Block3 Tim. 2 Block5 Tim. 1 25 - E Block5 Tim. 2 20 15 M Block8 Tim. 1 10 - M Block8 Tim. 2 5- M, 111111 RM VIA, 0- BlocklO Tim. 1 6 Intersection Figure 3.5.1.16 100 * BlocklO Tim. 2 per Aircraft Cia Average Intersection Crossing Times Block 1 15 12- 0 * 6 8 Intersection Figure 3.5.1.17 Average Intersection Crossing Times per Aircraft Class * Avg. T1 Heavy o Avg. T2 Heavy Block 2 Stdev T1 Heavy Stdev T2 Heavy Avg. Ti Large 0 Avg. T2 Large Stdev T1 Large -x Stdev T2 Large Avg. T1 Small E Avg. T2 Small Intersection Figure 3.5.1.18 101 * Stdev T1 Small Average Intersection Crossing Times per Aircraft Class Block 4 O Avg. TI Heavy Avg. T2 Heavy Stdev TI Heavy Stdev T2 Heavy Avg. Ti Large E Avg. T2 Large * Stdev T1 Large Stdev T2 Large Avg. Ti Small 4 Avg. T2 Small 9 Intersection Stdev T1 Small Figure 3.5.1.19 Average Intersection Crossing Times per Aircraft Class Block 5 N Avg. TI Heavy E3 Avg. T2 Heavy Stdev Ti Heavy Stdev T2 Heavy Avg. TI Large Ei Avg. T2 Large E Stdev Ti Large 01 Stdev T2 Large * Avg. T1 Small 3 7 8 Intersection Figure 3.5.1.20 102 * Avg. T2 Small * Stdev T1 Small 3.5.2 Intersection Use The following table provides information about the number of aircraft that used each intersection. Figures 3.5.2.1 through 3.5.2.4 show the intersection use under the four most popular runway configurations at Logan airport. As we can see, the use of a specific exit is closely related to the operating runway configuration. Number of Aircraft Using Each Intersection Intersection Block Block Block Block Block Block Block Block Block Block 1 2 3 4 5 6 7 8 9 10 1 0 2 0 0 6 0 0 0 1 0 2 0 15 0 0 23 0 0 0 0 0 3 0 5 0 4 21 0 -7 0 0 0 4 0 2 0 12 1 0 9 0 0 5 0 13 3 0 1 0 0 1 0 0 4 6 13 4 25 2 7 26 0 36 6 45 7 0 18 0 7 16 1 6 1 1 1 8 11 6 3 5 20 3 11 3 11 4 9 8 30 0 11 50 0 11 2 6 10 0 9 2 0 1 0 0 3 0 3 1 11 0 3 2 0 0 0 1 4 0 5 12 11 0 6 25 0 9 7 8 9 3 13 4 0 1 4 1 3 2 7 1 6 14 11 1 1 11 0 10 3 5 8 0 Table 3.5.2 103 Number of Aircrafts Using Each Intersection Configuration: Arrivals 4R, 4L and Departures 9. 4L Block1 0Block6 Block9 I C14 en IT I M %10 W t- 00 a I 0 Ch - ".4 - -4 Intersection Number Figure 3.5.2.1 Number of Aircrafts Using Each Intersection Configuration: Arrivals 33L and Departures 33L, 22R 50 45 40- - Block2 35 - 0 Block5 30. 25 20 - 15 10 - ft I 0 I - I e~ ~ - ~ -i I ~ I mr~ iE~ I ~.O t-= 00 Intersection Number Figure 3.5.2.2 104 0 - I 1 M 111111111111101110111111, M1111,ji I H III d . ... Number of Aircrafts Using Each Intersection III Configration: Arrivals 27, 22L and Departures 22R, 22L i ______________________________________ ________________________________ I MBlock3 Block8 BlocklO Z ru..11 J MJ I "- e.14 en %n~ 1.0 t- 00 ON 0- .4 - 1 - M~e - V- Intersection Number Figure 3.5.2.3 Number of Aircrafts Using Each Intersection Configuration: Arrivals 15R and Departures 9, 15R 50 45,, U 40m Block4 35 .E3 Block7 30 25 - S20 E 15 S10 1 5 Intersection Number Figure 3.5.2.4 105 W IiII 3.6 Taxiway Analysis 3.6.1 Taxiway Average Velocity The average velocity of an aircraft moving on an airport taxiway system depends on many factors. Before the analysis of the collected data, we expected that the distance of the taxiing segment would be a significant determinant of this velocity. Usually when pilots are moving on a short segment, prefer to taxi slowly since they expect soon to arrive at an intersection and might be instructed by the controller to stop for crossing traffic. On the other hand when a pilot sees that he has a long stretch in front of him with no imminent intersection, he taxies at higher speeds. The location of the taxiway segment should also play an important role. Taxiways far away from the terminal area are more likely to exhibit higher average velocities since they tend to be less congested and their surrounding areas are usually free of obstacles. Other variables that affect the taxiway velocities, are the complexity of the taxiway system at the particular airport and the level of familiarity that each pilot, who operates there, has with the system. The first variable usually remains constant while the second one can vary, and cannot be very easily quantified. Trying to test if the taxiway length and location relates to the average taxiway velocity, we categorized each taxiway link that did not belong to a runway or was not an exit link, into two groups. Those links that were shorter than 500 meters were assigned a letter S and those that were longer a letter L. Each taxiway was also assigned either a letter C (close) if it was located inside the outer taxilane, or a letter F (far) otherwise. 106 Id 1,14 , , j1 '1411 11, 1,111" '1 Figure 3.6.1.1 shows the average velocity of all taxiways for each data block independent of segment length or location. The velocities range between 7 and 16 knots. However, standard deviations vary from 6 to 22 knots. Data block 3 exhibits the lowest average velocity for its taxiways (7 knots), possibly due to the heavy traffic of that time period. To traffic congestion can be also attributed the low velocities that we observe in data block 4. Bad weather conditions (thunderstorms and fog) are the probable reasons for low velocities in blocks 1 and 9. Average Velocity in Taxiways 35 30. Mean 25 Stdev. 20 1 2 3 4 5 6 7 8 9 10 Data Block Figure 3.6.1.1 The results of the previous taxiway categorization can be seen in figures 3.6.1.2 and 3.6.1.3. Longer segments almost always display higher average velocities than the shorter ones. We must note though that in periods of heavy traffic the differences in speed between longer and shorter taxiways become smaller. As figure 3.6.1.3 shows, taxiways that are located far from the terminal area, in data blocks 1, 6, 9, 4 and 7, have higher average velocities while in the other blocks lower. It is interesting to note that blocks that have higher velocities, the runway configuration is the same (block 1, 6, 9 arrivals in 4R 107 departures from 9). The same pattern (same configuration for all blocks that exhibit similar velocity characteristics) occurs in the other blocks of data, where the combination (higher velocity - taxiway location) is opposite. I Length : Short I Long Average Velocity in Taxiways 35 0 30 25 20 4 I II o Sd Short I 15 , * Mean Short I I Mean Long S10 Sd Long 5 0 .3 N en~ IT in vC r- 00 o 0 Data Block Figure 3.6.1.2 Figure 3.6.1.4 shows two groups of taxiways. In the first group, belong taxiways that are located close to the terminal area and are short in length, while in the second one the taxiways that are located further away and are longer. Here, the differences in velocities between the far and long and the close and short becomes even larger in favor of the longer and further away ones compared to the previous two figures. However, these differences, in the blocks where close and short taxiways have higher velocities, become smaller. Overall, we can conclude that there exist a close relationship between the length of the taxiway and the taxiing velocity. The location of the taxiway segment seems to be also critical. We must also note that traffic congestion has a more deleterious effect on the average taxiing velocity than bad weather conditions. 108 Average Velocity in Taxiways Location Close / Par i0 Mean Close Sd Close Mean Far 0 * Sd Sd Far Fa 'U Eu 0 W-4 Cq n "t Dtna- Bo %0 00 0 Data Block Figure 3.6.1.3 Average Velocity in Taxiways Location: Close I Par Length: Short / Long 35 W 130- Mean C &S S25- 0 Sd S20- 15- Mean F &L n asU &S t0 SdF&L S5 0 Data Block Figure 3.6.1.4 109 3.6.2 Taxiway Use Figure 3.6.2.1 through 3.6.2.10 present the use of the taxiway segments that constitute the inner and outer taxilanes. All data blocks show an almost identical taxiway use no matter what is the runway configuration. The most often used taxiway links are B03-B04 and B04-B05 of the inner taxilane. Only block 3 demonstrates a higher percentage wise use of the outer taxilane, probably due to the heavy surface traffic of that day. In figure 3.6.2.11 through 3.6.2.20 the use of the supporting taxiways is presented. As supporting taxiways are classified all the taxiway links that do not belong to either a runway or the inner and outer taxilanes, but feed traffic to the terminal and runway areas. A very strong relationship between the use of the these taxiway links and the particular runway configuration seem to exist, as figures of data blocks with the same configuration seem identical. 110 'TI B08A92 B09A93 A50A20 A35A42 A97A98 A98A80 A80A99 A99B00 BOOBO BO1B02 B02B03 B03B04 B04B05 B05B06 B06B07 B07B08 B08B09 B09A95 A95A96 A97A79 A79A81 A81BIO B10A82 A82A83 A83A84 A84A85 A85A86 A86A70 A70A60 A60AOO AOOA1O A1OA20 A50A91 A91A92 A92A93 A93A94 A94A95 Number of Aircraft B08A92 B09A93 A50A20 A35A42 A97A98 A98A80 A80A99 A99B00 BOOBO BOIB02 B02B03 B03B04 B04B05 B05B06 B06B07 B07B08 B08B09 B09A95 A95A96 A97A79 A79A81 A81B1O B10A82 A82A83 A83A84 A84A85 A85A86 A86A70 A70A60 A60AOO AOOA1O A1OA20 A50A91 A91A92 A92A93 A93A94 A94A95 0) tA 0 U Number of Aircraft r .. A79A81 A81B10 B10A82 ... A82A83 A83A84 ----A84A85 ... A85A86 A86A70 A70A60....x. A60A0O AOOAO .... A1OA20 A50A91 ... A91A92 A92A93 A93A94 A94A95 A97A79 B08B09 B09A95 A95A96 B07B08 B05B06 B06B07 B03B04 B04B05 B09A93 A50A20 A35A42 A97A98 A98A80 A80A99....... A99B00 BOOBOI B01B02 B08A92 Number of Aircraft 9 - 0% ~ - ~1. B08A92 B09A93 A50A20 A35A42 A97A98 A98A80 A80A99 A99B00 BOOBOI BO1B02 B02B03 B03B04 B04B05 B05B06 B06B07 B07B08 B08B09 B09A95 SA95A96 A97A79 t A79A81 A81BIO B10A82 A82A83 A83A84 A84A85 A85A86 A86A70 A70A60 A60AOO AOOA1O A1OA20 A50A91 A91A92 A92A93 A93A94 A94A95 C: 8 s 8 C8t Number of Aircraft B08A92 B09A93 A50A20 A35A42 A97A98 A98A80 A80A99 A99B00 BOOBOI BO1B02 B02B03 B03B04 B04B05 B05B06 B06BO7 B07B08 B08B09 B09A95 A95A96 A97A79 A79A81 A8B1O B1OA82 A82A83 A83A84 A84A85 A85A86 A86A70 A70A60 A60AOO AOOA1O A1OA20 A50A91 A91A92 A92A93 A93A94 A94A95 ... ..... .. . . . " . """""""""...... ................................................... Number of Aircraft to - 96 - C -I O|l x t S A79A81 A81B1O B10A82 A82A83 A83A84 A84A85 A85A86 A86A70 A70A60 A60A00 AOOA10 A1OA20 A50A91 A91A92 A92A93 A93A94 A94A95 A97A79 B02B03 B03B04 B04B05 B05B06 B06B07 B07B08 B08BO9 B09A95 A95A96 B01B02- B08A92 B09A93 A50A20 A35A42 A97A98 A98A80 A80A99 A99B00 B300B301 BOOBOI ---- ----- -====..-.-.. ....... . Number of Aircraft (D :: I m " g A95A96 A97A79 A79A81 A8iBIO B10A82 A82A83 A83A84 A84A85 A85A86 A86A70 A70A60 A60AOO A00A1 A1OA20 A50A91 A91A92 A92A93 A93A94 A94A95 SB09A95 B053B06 B06B07 B07B08 B08B09 B --------... -.........----..........--. --. ............... BO8A92 B09A93 A50A20 .------A35A42 -----A97A98 A98A80 A80A99. A99B00 . B00301 ......... B01B02 .... B302B03 -- Number of Aircraft * - -j A80B10 A20A40 A39A37 A37A31 B04A60 A18A24 A16A17 A33A32 A32A31 A18A19 A02AO1 A02A04 A04A07 A07A90 B06A1O A35A43 A44A43 B03A70 A48A47 B14B13 A98A81 B00A83 A74A73 A73A71 A71A69 A67A66 A66A63 B02A86 A99A82 B05AOO A35B13 A34A33 B06A50 .......... o C0L C *- ssa e s : Pt o 0 ~J ------------------------------------ LA-/ Number of Aircraft - - B06A50 A34A33 A35B13 B05AOO A99A82 B02A86 A66A63 A67A66 - - - - - - - A73A71 A71A69 - A74A73 - A98A81 B00A83 B14B13 A48A47 B03A70 A44A43 * A35A43 A07A90 " B06A1O A02AO1 A02A04 A04A07 A18A19 " A32A31 A33A32 B04A60 A18A24 A16A 17 A37A31 ASOB1O A20A40 A39A37 "g p 0 I U .A o ~ k~ 0 ~Jm Number of Aircraft 0 ~Ju - 9 ~1. A80BO A20A40 A39A37 A37A31 B04A60 A18A24 A16A17 A33A32 A32A31 A18A19 A02AO1 A02A04 A04A07 A07A90 B06AIO A35A43 A44A43 B03A70 A48A47 B14B13 A98A81 B00A83 A74A73 A73A71 A71A69 A67A66 A66A63 B02A86 A99A82 B05AOO A35B13 A34A33 B06A50 Ig .:.:.; ........ U 0.A0 IN)3 0 ~A 0 ~A -------------MM tJm - Number of Aircraft 0 A80B1O A20A40 A39A37 A37A31 B04A60 A18A24 A16A17 A33A32 A32A31 A18A19 A02AO1 A02A04 A04A07 A07A90 B06A1O A35A43 A44A43 B03A70 A48A47 B14B13 A98A81 B00A83 A74A73 A73A71 A71A69 A67A66 A66A63 B02A86 A99A82 B05AOO A35B13 A34A33 B06A50 0 ~A 0 I M ~ 3 RON Pg 1-" Number of Aircraft 00 -*9 021 A80B1O A20A40 A39A37 A37A31 B04A60 A18A24 A16A17 A33A32 A32A31 A18A19 A02AO1 A02A04 A04A07 A07A90 B06A10 A35A43 A44A43 B03A70 A48A47 B14B13 A98A81 B00A83 A74A73 A73A71 A71A69 A67A66 A66A63 B02A86 A99A82 B05AOO A35B13 A34A33 B06A50 0 ~ I o - U U ~A LA 0 ---------- 0) Number of Aircraft A8OB10 A20A40 A39A37 A37A31 B04A60 A18A24 A16A17 A33A32 A32A31 A18A19 A02AO1 A02A04 A04A07 A07A90 B06A1O A35A43 A44A43 B03A70 A48A47 B14B13 A98A81 B00A83 A74A73 A73A71 A71A69 A67A66 A66A63 B02A86 A99A82 B05AOO A35B13 A34A33 B06A50 U ti i ~ [ I ............ ............. U 7:..... 7 ........ . .................. .... . .......... ........ .. ........ ............ ....... ............. - Number of Aircraft A18A24 A16A17 A33A32 A32A31 A18A19 A02AO1 A02A04 A04A07 A07A90 B06A10 A35A43 A44A43 B03A70 A48A47 B14B13 A98A81 B00A83 A74A73 A73A71 A71A69 A67A66 A66A63 B02A86 A99A82 B05AOO A35B13 A34A33 B06A50 B04A60 A80BIO A20A40 I A39A37 A37A31 I * I- U - Number of Aircraft T_ A35B13 A34A33 B06A50 B05AOO A99A82 B02A86 A66A63" A71A69 A67A66 A73A71 - - - - A80B1O A20A40 A39A37 A37A31 B04A60 A18A24 A16A17 A33A32 A32A31 7 A18A19 A02AO1 A02A04 A04A07 A07A90 B06A10 A35A43 A44A43 B03A70 A48A47 B14B13 " A98A81 B00A83 A74A73 Z Ot) 00O) -I.." :MEMO I II CA Number of Aircraft A73A71 A71A69 A67A66 A66A63 B02A86 A99A82 B05AOO A35B13 A34A33 B06A50 A74A73 A48A47 B14B13 A98A81 B00A83 B03A70 A07A90 BO6A10 A35A43 A44A43 A04A07 A02A04 A16A17 A33A32 A32A31 A18A19 A18A24 A80B1O A20A40 A39A37 A37A31 B04A60 Aircraft .............. Number F pr A8OB1O A20A40 A39A37 A37A31 B04A60 A18A24 A16A17 A33A32 A32A31 A18A19 A02AO1 A02A04 A04A07 A07A90 BO6A1O A35A43 A44A43 B03A70 A48A47 B14B13 A98A81 B00A83 A74A73 A73A71 A71A69 A67A66 A66A63 B02A86 A99A82 B05AOO A35B13 A34A33 B06A50 I p & Number of Aircraft Chapter 4 Conclusions 4.1 Introduction In this chapter the major observations of the previous analyses are discussed and final conclusions are drawn. These conclusions are divided into three sections; runways, intersections and taxiways. Finally, the last part provides some directions for future research. 121 4.2 Runways The runway analysis showed some interesting results. The occupancy time on landing does vary, as expected, with aircraft size but this variation is mainly due to the fact that heavier aircraft tend to exit further down the runway, resulting in higher occupancy times. However, aircraft using a given exit have similar occupancy time, independently of aircraft size. The particular angle of the exit used also plays a very significant role. Aircraft that use obtuse angled exits, usually exit at higher speeds, and therefore maintain a higher average landing velocity resulting in similar occupancy times compared to exits that are located much closer to the runway threshold. The standard deviation of the occupancy time is usually smaller for aircraft using the first exits, than those exiting further down the runway. Visibility also affected the occupancy time, mainly due to the increased use of exits located further down the runway. In similar weather conditions, aircraft using exit 6 (high speed) of runway 27, in day light had average occupancy times of 35 seconds (lowest overall), while at night, in similar weather conditions, most aircraft used exit 8 (low speed) and their occupancy times were significantly increased (53 seconds). In the analysis of exit usage, as mentioned above, heavier aircraft tend to use exits located further away from the threshold, while smaller sized ones require shorter landing distances and exit earlier. The specific turning angle of the exit was also a determinant factor of its use. As a result, independently of runway, most aircraft tended to prefer the use of obtuse angled (high speed) exits. Exit velocities, as expected, were closely related to the angle of the exit, and whenever aircraft where using obtuse angled exits they exited at significantly higher speeds. However, this was only true, for high speed exits that were accompanied with 122 long exit segments and allowed the pilot enough distance to brake. The exit velocity did not vary uniformly between aircraft classes and it seemed that exit velocity does not depend on aircraft size. The landing velocity profiles showed a close relationship between the amount of deceleration and the type of exit (high or low speed) used after landing. In the final approach, we observed a slight deceleration as the aircraft were approaching the threshold. Data from runway 27, illustrated the importance of visibility, as in day light, this deceleration was quite significant whereas during night operations we saw a much smoother final approach profile. In runway 15R, under different weather conditions, aircraft seem to even accelerate before the threshold. 4.3 Intersections There is a significant difference in average crossing time depending in the runway configuration and thus in the direction of use of some intersections. For example, when intersections 10, 11, 12, 13 and 14 are used in the inbound direction (towards the terminal area), usually after arrivals in runway 27, the crossing times seem to be much smaller compared to those of departing aircraft which use the same intersections but in the opposite direction (outbound), and often have to form a queue while waiting to depart from runway 9 and thus cross these intersections very slowly. Comparing the crossing times of the two different segments of each intersection (time 1 and time 2), we observe that usually when an intersection is used in the inbound direction time 2 is larger than time 1 and when it used in the outbound time 1 is larger. This could be due to the fact that often pilots slow down and approach the terminal area 123 cautiously, while on their way to the departing runway, they accelerate faster out of an intersection since the taxiways that lead away from the terminal are usually longer. Aircraft size did not seem to be a determinant of crossing times as larger size aircraft had longer crossing times only in few blocks. Exit usage was closely tied to the operating runway configuration. 4.4 Taxiways In the taxiway analysis we saw that there exists a close relationship between the length of the taxiway and its velocity. Taxiways far away from the terminal almost always exhibit higher average velocities since they tend to be less congested and free of surrounding obstacles. We must note though, that in periods of heavy traffic the differences in speed between longer and shorter taxiways become smaller. The use of the inner and outer taxilanes under different configurations is almost identical. However, a very strong relationship between the use of the supporting taxiways around the terminal area, and the particular runway configuration seems to exist. 4.5 Directions for Future Research Although after the analysis of the data many questions regarding the motion characteristics of aircraft moving on the surface of Logan airport have been answered, many more have been raised. More research should be done on the factors that affect airport surface traffic in order to successfully develop and implement future surface 124 traffic automation systems. This study was limited to only Logan airport but a future one should include and compare data from a wide variety of airports. Such a study could include analysis of other variables that affect surface traffic such as congestion and examine in further detail their potential effects. Most importantly, a much larger size of data must be gathered. This requires some form of radar surveillance at the airport. In our case, even though almost 12 hours of airport operation data were made available for this study, after the breakdown of all aircraft by aircraft type, runway and exit used we were left with very small sample for each variable that we wanted to measure, limiting the accuracy of our results. There is much more data available for Logan if further confidence in the measurements is required. Hopefully, the content of this thesis will act a catalyst in attracting interest and consequently, more studies will be under taken in the future, for a more complete understanding of the surface traffic variables and a more efficient use of the airport surface. 125 References 1. Bussolari, Steven (1991), Real-Time Control Tower SimulationforEvaluation of Airport Surface Traffic Automation, International Symposium on Aviation Psychology Proceedings Vol. 1 (A92-4401) 2. 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