C-Nav GPS: Confidence Through Diversity Eliminating the need for multiple vendor solutions C-Nav’s advanced positioning solutions deliver real-time decimetric Precise Point Positioning to the international maritime community. In addition to the C-Nav NET-1™ network, C-Nav GcGPS now offers a second network, C-Nav NET-2™, an additional positioning layer providing independent integrity checks and back-up for customers requiring two independent solutions. By working with industry and its partners, and through the technological expertise of its engineers, C-Nav has been able to drive down costs to the point where a dual C-Nav system is substantially less than the cost of having two different vendors’ systems. For the first time, this allows a wider range of GNSS positioning users to benefit from the advantages of integrity confidence. NET-1 and NET-2 use C-Nav’s proprietary worldwide tracking and monitoring network augmented by sites within the Jet Propulsion Laboratory (JPL) tracking network. This paper introduces the unique concept of full system redundancy, integral QC, and accuracy monitoring through spatial and processing diversity. *** With the addition of C-Nav NET-2, the C-Nav GcGPS system now benefits from a monitoring capability equivalent to having Fugro’s Starfix XP on board but with accuracy and robustness identical to that of C-Nav NET-1. Until now, most independent integrity checks utilized dGNSS solutions from two separate vendors. These were considered wholly ‘independent’ but of similar order. But in practice, no two dGNSS systems can be fully independent. All vendors share common elements including the satellite constellations, broadcast integrity information, and the satellite clock and ephemeris data. Errors or integrity issues at this level are system-common and community shared. Some commercial dGNSS and augmented GNSS system vendors also share tracking networks. C-Nav NET-1, and C-Nav NET-2, Fugro’s XP, and Veripos Ultra use the Jet Propulsion Laboratory (JPL) tracking sites. C-Nav, additionally, incorporates proprietary tracking and monitoring stations providing the user with built-in redundancy. Because of the heavier concentration of sites, the system is far less prone to the effects of spatial decorrelation should an isolated episode occur at any single site. In contrast with conventional DGPS systems, where error and failure at the reference sites can seriously impede the position solution, C-Nav’s service is based on a worldwide overdeterminate tracking network for Precise Point Positioning (P3) utilizing orbit and clock correctors for all GPS satellites. C-Nav has the exclusive benefit of generating and applying the satellite orbit and clock correctors tightly modelled in an integrated RTG solution. The vulnerability of system failure is mitigated by redundancy through route diversity and system backups. This robust C-Nav structure provides redundancy at each layer. For example: © 2008 C&C Technologies, Inc. and its partners. All rights reserved. confidence thru diversity rev 3.0.1.doc Page 1 • Tracking stations have a 6:1 excess ratio; stations can be removed from the solution if their data is questionable or inaccessible without affecting system performance. • NET-1 and NET-2 provide independent communication links between the hubs and the system users. • All C-Nav tracking stations have dual racks of equipment. In the event that performance becomes questionable, a rack can be excluded without impacting the solution. • Each C-Nav tracking station has multiple communication links to the Processing Centers. In the event of a communications failure, an alternate method of communication is automatically put on line. • Each system user may employ multiple and / or differing C-Nav receivers. REAL-TIME GIPSY® (RTG) Inherent errors and limitations associated with traditional DGPS reference stations are eliminated with the C-Nav enhanced RTG solution. Operating at the fundamental GPS level, each GPS satellite error source is evaluated independently - a major advance beyond earlier DGPS ground-based augmentation systems. The C-Nav ground infrastructure includes a global network of satellite tracking and systemmonitoring sites providing a quality controlled feedback loop. Two dedicated and independent Processing Centers each employ an advanced proprietary version of the Jet Propulsion Laboratory’s Real-Time GIPSY® (RTG) software. The Processing Centers ensure that the six fully redundant L-band hi-power communication satellites distribute validated correction data to C-Nav’s worldwide user community. Table 1, C-Nav RTG - GNSS Fundamental Augmentation Configuration: Correction Satellite orbit Satellite clock Atmospherics Multi-path Receiver Earth Tides Implementation 1 Minute RTG 1-2 Second RTG C-Nav L1/L2 Receiver Hardware Multi-Path Mitigation Software (patented) and antenna technology C-Nav 16 channel L1/L2/L-band hardware Sinko’s model and ocean loading incorporated in the receiver C-Nav’s GNSS comprises of four main segments: − GROUND: Global network of reference stations and integrity monitors − CONTROL: Orbit and clock processing − SPACE: Signal distribution − USER: Data acquisition and application (receivers), plus access to system monitor network updated every minute from the C-Nav website GROUND SEGMENT The C-Nav ground network comprises of reference / monitor stations equipped with two dualfrequency GPS receivers (each hereafter referred to as ‘Receiver A’ and ‘Receiver B’). The © 2008 C&C Technologies, Inc. and its partners. All rights reserved. confidence thru diversity rev 3.0.1.doc Page 2 observations from both receivers are transmitted to the two Processing Centers. Selected stations within the network are additionally equipped with dual-frequency user hardware to monitor the L-Band signal strength to measure and compare real-time position, accuracy, and precision. The number of GNSS receivers at each ground station, compounded by the number of simultaneous observations from each GNSS satellite by the station network (typically better than seven), and augmented by the JPL ground network provides an unprecedented level of over-capacity and system robustness. Each C-Nav station is located within a secure facility, with secure communication data links to the control segment, and backed up by VSAT or ISDN and uninterruptable power supplies. Table 2, reference / monitor stations (April 2008): 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 Antarctica, Ross Island Argentina, Rosario Australia, Brisbane Australia, Sydney Australia, Melbourne Australia, Perth – C Australia, Perth – M Australia, Tidbinbilla Brazil, Catalão Brazil, Horizontina Brazil, Sapezal Diego Garcia Chile, Santiago China, Jiamusi Colombia, Bogota Cook Islands, Rarotonga Ecuador, Galapagos Finland, Tampere Germany, Zweibrucken Greenland, Kellyville Guam, Dededo India, Bangalore 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 Japan, Tokyo Japan, Usuda Kyrghystan, Bishkek Netherlands, Burum Netherlands, Delft New Z’land, Auckland Peru, Arequipa Philippines, Quezon City Russia, Irkutsk Russia, Moscow Russia, Norilsk Russia, Petpropavlovsk Russia, Urals Ridge Russia, Yakutsk S Africa, Johannesburg S Africa, Krugersdorp S Africa, Sutherland Spain, Madrid Spain, Madrid Uganda, Mbarara USA, Fairbanks USA, Torrance 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 USA, USA, USA, USA, USA, USA, USA, USA, USA, USA, USA, USA, USA, USA, USA, USA, USA, USA, USA, USA, USA, USA, Goldstone Pasadena (JPL) Pasadena (JPL) Quincy Colorado Springs NIST, Boulder Belle Glade Mauna Kea Kokee Park Moline Greenbelt Fargo Pietown Syracuse Lamont Portland Puerto Rico Weslaco Christiansted Brewster Woodinville USNO Master Clock Each GPS satellite is tracked by multiple Reference / Monitor Stations and can maintain P3 precision even with a number of stations out of commission (an event that has never happened). This level of over-capacity will soon be further improved when the next generation of C-Nav RTG precision is introduced. CONTROL SEGMENT The control segment comprises two independent Processing Centers, each fitted with dual sets of processing hardware. One center is located in Torrance, California and the other in Moline, Illinois. The Processing Centers are interconnected by high-speed frame-relay feeds and receive the full complement of reference station data. Each Processing Center makes an independent selection between Receiver A and Receiver B, producing independent sets of RTG correction values for each GPS SV. After the Processing Centers have exchanged and compared their correctors for validation, each sends its correctors independently to the Land Earth Stations (LES) for uplink to the NET-1 and NET-2 © 2008 C&C Technologies, Inc. and its partners. All rights reserved. confidence thru diversity rev 3.0.1.doc Page 3 communication satellite constellations. Data flow between the Control Centers and the Land Earth Stations is via secure high-speed cable and VSAT with ISDN backups. SPACE SEGMENT: NET-1 & NET-2 Figure 1 C-Nav NET-1 and NET-2 world coverage The C-Nav space segment consists of six geostationary communication satellites providing redundant Hi-power L-Band distribution between approximately 75° north and 75° south latitudes. The six communication satellites are constantly monitored by the Processing Centers to ensure service continuity. Additionally, various ground stations monitor the received L-Band signal strength to confirm satellite transmission signal levels, veracity, and precision of received data. The satellite constellation is up-linked through six Land Earth Stations configured as NET-1 and NET-2. Table 4, C-Nav’s six geostationary communication satellites: Land Earth Station Satellite Satellite longitude NET-1 Laurentides, Canada Burum, NL Perth, WA Inmarsat High Power Inmarsat High Power Inmarsat High Power Santa Paula, Ca, USA Southbury, Cn, USA Auckland, NZ Inmarsat High Power Inmarsat High Power Inmarsat High Power 98°W 25°E 109°E NET-2 142°W 15.5°W 143.5°E USER SEGMENT RECEIVER TECHNOLOGY C-Nav2050: © 2008 C&C Technologies, Inc. and its partners. All rights reserved. confidence thru diversity rev 3.0.1.doc Page 2 At the heart of every C-Nav2050 dual-frequency receiver is the Touchstone-4 ASIC. This 26channel dual-frequency receiver is integrated with a proprietary L-Band receiver and tri-band antenna. C-Nav2050 dual-frequency receivers measure the ionospheric delay for each satellite while the tropospheric zenith delays are calculated from a multi-state time and position model aided by redundant satellite observables. Typically, a C-Nav2050 dual-frequency receiver operating on NET-1 or NET-2 will provide better than 10 cm horizontal and 15 cm vertical accuracy. Unlike DGPS positions that are relative to reference station locations, C-Nav produces absolute ITRF 2005 positions, within geostationary satellite visibility, anywhere, any time. C-Nav1010: The latest addition to the C-Nav hardware line-up is the CNav1010 L1 receiver. In common with the rest of the C-Nav family of receivers, it integrates the C-Nav correctors in addition to WAAS / EGNOS data. The C-Nav1010 is a tightly integrated package designed to maximize precision and stability in noisy and hostile environments. Offering submeter accuracy worldwide, and at a lower cost than the highperformance 2050, the 1010 is a rugged and reliable unit designed for maximum productivity with minimal setup time. C-Nav2000: The C-Nav2000 is a ‘smart-antenna’ design with an integrated dual-frequency GPS, L-Band demodulator, and a tri-band antenna in one package. The C-Nav2000 remains a key product for surveyors requiring two independent dual-frequency C-Nav solutions. The C-Nav2000 was introduced to the marine market in 2000. Although no longer manufactured, there are many hundreds of C-Nav2000 units working in the international marine market with lease units available through survey equipment suppliers. SUMMARY The C-Nav Precise Point Positioning solution has been purpose-designed to provide the marine sector with the most accurate, reliable, and integrity-independent dGNSS system in the world. The addition of C-Nav NET-2 to the worldwide C-Nav gcGPS network provides additional levels of security, integrity and confidence to an already resilient and well-managed network. C-Nav GPS receivers can be licensed to operate using NET-1 or NET-2 correction signals either individually or with both Networks to provide maximum reliability and technical redundancy. Vessels can be equipped with two separate C-Nav positioning systems; one dedicated to NET-1 and the other to NET-2 providing two independent delivery solutions. © 2008 C&C Technologies, Inc. and its partners. All rights reserved. confidence thru diversity rev 3.0.1.doc Page 3 Choices of three different integrated receivers are also available. Incorporating different GPS engines, each receiver provides the user with exceptional options for independent system selection, comparison, confidence, and integrity. C-Nav element Ground segment Redundancy 66 stations (excess ratio 6:1) Communications (to/from Control Centers) Processing Centers Satellites Robustness Independent measurements Solutions RTG measures and real-time monitoring Multi-routes with ISDN back-up 2x on-line + 1x (independently operated) back-up Independent selection of A or B reference receivers Communications (to/from LES) Land Earth Stations Resilience 2x receivers per CNav station 2x production layers / Control Center Independent RTG generation / Processing Centre Independence 2x RTG generation and Real-Time monitoring Multi-routes + VSAT with ISDN back-up Minimum 2x LES per Ocean Region NET-1 & NET-2 Independent selection of RTG correctors for 2x production layers uplink i.e. four / LES permutations per Ocean Region Minimum 2 Satellites per Ocean Region. NET-1 & NET-2 Standby channels on back-up SVs Example user hardware permutations Receivers / user configurations NET-1 NET-2 1 2 3 4 5 6 7 2x 2050 1x 2050 1x 2050 1x 1010 2x 1010 1 x 2000 1x 2050 2x 2050 1x 1010 1x 2050 2x 1010 1 x 2050 Real-Time monitoring RTG WAAS/EGNOS RTK 2050 / 1010 / 2000 2050 / 1010 2050 / 1010 2050 / 1010 2050 / 1010 2050 / 2000 1010 © 2008 C&C Technologies, Inc. and its partners. All rights reserved. confidence thru diversity rev 3.0.1.doc Page 4