ROBOTIC AIRCRAFT FOR PUBLIC SAFETY (RAPS) OVERVIEW Kirk Kloeppel 20 March 2014 UAS or “DRONE” 2 Contents • RAPS Purpose, Approach, Scope • Test Range • Process ̶ Manufacturer Participation ̶ Performance Goals ̶ Test Plan ̶ Test Reports • Schedule, Lessons Learned, Future Outlook • Web Links • Back Up Information 3 Purpose/Test Approach • To evaluate performance and utility of SUAS-sensor combinations using: ̶ Key capability measures ̶ One test – ours – applied uniformly to all systems to be tested ̶ Realistic operational test scenarios and environments ̶ Test reports produced for each system tested • Primary focus: Capability gaps of public, first responder organizations ̶ All levels of government, including DHS operational components, especially Customs and Border Protection Office of Border Patrol; U.S. Coast Guard; USSS; FEMA; other – Many other stakeholders/partners: FAA; DOJ/FBI, DJP; DOS/AVC-VTT; DOC/NOAA, NIST; NASA; DOD; DOI/NFS, NPS, USGS; CAL FIRE; other 4 RAPS Scope • Test categories ̶ Scripted operational scenarios – Search and rescue (SAR) – Fire/HAZMAT/disaster – Law enforcement (LE) ̶ Operational utility assessments ̶ Use in National Airspace System (NAS) Technical scope, requirements ̶ Restricted airspace (COAs are not feasible) ̶ Fixed- and rotary-winged aircraft, < 25 lb MTOW, and modular, available sensors (already integrated) that address our test objectives ̶ Day-time flight testing at altitudes < 400 ft (AGL) 5 Air-based Tech R&D • Other research and development activities ̶ RAMPS is a new S&T-USCG Research and Development Center (RDC) partnership for SUAS Maritime testing ̶ Technology foraging and field testing – Severe storm modeling and simulation – Airborne collision avoidance – Counter-spoofing/jamming ̶ Ongoing support to DHS’s Working Group on Privacy and Civil Rights and Civil Liberties ̶ U.S. border security demonstration √ ̶ Ultra-quiet SUAS prototype √ 6 Border Security Benefits – Rapid response ̶ ̶ Improved situational awareness and agent safety High-value assets in remote, inaccessible, dangerous AORs – Relatively low unit costs could provide ̶ ̶ Many more air assets for target identification and tracking Eventually, complete aerial coverage of the U.S. border 7 7 RAPS Test Range Oklahoma Training Center – Unmanned Systems (OTC-US) Location: Elgin, OK, adjacent to Ft. Sill U.S. Army Post and within Ft. Sill restricted airspace OTC-US site (red outline) OTC-US is a test facility of the Oklahoma State University’s University Multispectral Laboratory “Liberty City” site (urban scenarios) 8 Vendor Participation • We developed 21 SUAS Performance Goals ̶ ̶ Based on notional user scenarios created by senior LE, fire, SAR, and border security operators Scenarios were vetted with operational communities • Our Goals encompass: ̶ ̶ Areas noted: User applications; operational utility; transition to NAS RAPS PM priority to seek mature SUAS solutions that could support near-term transition of good (not necessarily the best) capabilities September 2012 RFI invited manufacturer participation (“Cycle 1”): 72 white papers were received ̶ White paper screening and selection process: Compliance check vs. RAPS Performance Goals Results: Near-term testing; Later testing; Rejected (non-compliant) 9 SUAS Performance Goals Common Requirements: Threshold Objective Lost Link Procedures Airframe Accumulated Flight Time Sensors Sensors (EO/IR) Laser Designation Training (operator) Deployment Recovery Assembly Ready to launch (after assembly) Mean time between lost link Airworthiness–Operator’s Manual Airworthiness–Maintenance Manual Weight (MTO) Rally Point > 200 hr (rotary); > 500 hr (fixed) Electro-optical and infrared Fixed None One week Bungee/catapult launch Line/net capture < 5 min < 5 min > 100 hr flight time Provide written Operator’s Manual Provide written Maintenance Manual < 25 pounds Rally Point, after time return to launch > 400 hr (rotary); > 1,000 hr (fixed) Chemical/biological/radiological Gimbaled Laser spotter integrated One day Hand launched Deep stall/hover < 1 min < 1 min > 250 hr flight time Provide written Operator’s Manual Provide written Maintenance Manual < 25 pounds Rotary-winged UAS: Threshold Objective Fixed-winged UAS: Threshold Objective Endurance Range Speed (dash) Speed (endurance) Altitude Service Ceiling Acoustic signature (400 ft AGL) Endurance Range Speed (dash) Speed (endurance) Altitude Service Ceiling Acoustic signature (400 ft AGL) 30 min 1 mi 20 mph 15 mph 400 ft AGL 6,000 ft MSL 70 dBA 2 hr 3 mi 40 mph 30 mph 1000 ft AGL 10,000 ft MSL 40 dBA 30 min 0.25 mi 10 mph 0 mph 400 ft AGL 6,000 ft MSL 70 dBA 1 hr 1 mi 30 mph 20 mph 1000 ft AGL 10,000 ft MSL 40 dBA 10 Test Plan • Test Plan uses standard methodologies for operational evaluation ̶ 54 Performance Measures (PMs) ̶ Approved for public release in 2012 ̶ A living document that considers ongoing consideration of stakeholder suggestions for improvements • “Cycle 1” is the current test program ̶ Future, “Cycle 2” testing (FY2015+), if approved, may or will encompass: • Expanded fire, SAR, disaster response scenarios • Specialized sensor testing • More complex test scenarios (example: marine, riverine testing) • Airworthiness criteria 11 Key Test Factors • Operational capabilities ̶ Does SUAS support routine operations by improving situational awareness? • Operational utility ̶ Is SUAS easy and efficient to assemble, launch, operate, recover, and pack up? ̶ Is video output seen effectively at multiple remote terminals? • Technology transition ̶ Is FAA authorization permitting SUAS operation in the NAS likely? 12 Test Reports • Reports ̶ ̶ Created by S&T RAPS team for users Vendors: (i) Perform fact checks of final draft; (ii) identify proprietary information; and (iii) clear Executive Summary for public release Approved for release by DHS S&T Posted and archived online ̶ ̶ • Websites ̶ ̶ Government employees and government-sponsored stakeholders access the Reports via http://www.firstresponder.gov, the gateway to S&T’s First Responder Communities of Practice site, https://communities.firstresponder.gov, which is the gateway to the RAPS Community of Practice site. Access controlled by S&T and RAPS PM 13 Test Reports, cont’d • Test Reports ̶ Content: Complete test results, including scoring summary tables; general SUAS information; company-proprietary cost and other information ̶ Audience: Restricted to government employees and government-sponsored stakeholders interested in RAPS (potential users) ̶ Access to Test Reports: • Available upon request to RAPS Program Manager • Available online at Robotic Aircraft for Public Safety (RAPS) Secure Community of Practice website • Executive Summaries of Test Reports ̶ Content: Highlights of test results ̶ Audience: Approved for public release (goal: to reach a wide readership) ̶ Access to Executive Summaries: • Available upon request to RAPS Program Manager • Available online at Robotic Aircraft for Public Safety (RAPS) Community of Practice website 14 Rating Summaries To facilitate SUAS comparisons, each Report contains Rating Summaries of results in our 54 Performance Measures in 5 Assessment categories: A1. Law Enforcement; A2. Search and Rescue; A3. Fire Response; A4. Operational Utility; A5. Operation in NAS Above: Sample Rating summary information Performance Measure (PM) Unit, Rating (bar-graph), T & O markers Qual., Quant. Rating Scoring Keys for Qualitative and Quantitative Ratings 15 RAPS Schedule (Cycle 1) 3 4 5 6 7 8 9 Lockheed Martin ADP AeroVironment Platform(s) Stalker (Blk 15), Stalker XE (Blk 10) Puma AE, Raven B, Wasp AE (Blk IV) Report Online 2 Dec. 10-14, 2012 Jan.14-18, 2013 Mar. 11-15, 2013 Apr. 15-19, 2013 May 13-17, 2013 June 10-14, 2013 June 17-21, 2013 July 15-19, 2013 Aug. 26-30, 2013 Company Rotary 1 Test Date Fixed Test Week √ √ √ √ T-Hawk (Blk II) √ √ Avenger; R.A.P.T.R. √ √ Aeryon Labs Scout V1, SkyRanger √ √ UAS Dynamics Skylark √ Lockheed Martin MS2 Desert Hawk III, Desert Hawk-EER, Indago √ Mission Technology Systems, LLC Buster √ AeroVironment Qube, Shrike Honeywell Leptron (Tactical Electronics) √ √ 16 RAPS Schedule (Cycle 1) 12 13 14 N/A 15 16 17 Company Platform(s) AirRobot AR100B, AR100C, AR200 Prioria Maverick, VMAV √ Falcon UAS Falcon √ Applied Research Assoc. Nighthawk √ AirCover/Lockheed Martin QR425 √ CBP (PSI Tactical) InstantEye √ UAV Solutions Talon, Allerion, Phoenix30 √ Stark Aerospace BirdEye 400, Mini-Panther √ Aurora Skate √ Report Online 11 Sept. 9-13, 2013 Oct. 21-25, 2013 Dec. 9-13, 2013 Jan. 13-17, 2014 Jan. 27-31, 2014 April 14-25, 2014 May 12-16, 2014 May 19-23, 2014 June 16-20, 2014 Rotary 10 Test Date Fixed Test Week √ √ √ 17 Lessons Learned – To Date • No one platform performs well in all scenarios • Fixed-wing aircraft: ̶ Very good in search and rescue (SAR), fire monitoring ̶ Some fixed wing SUAS need operating areas > 200 ft radius • Launch and recovery zones • Deep stall landings affected by winds • Rotary-winged aircraft: ̶ Perform well in crime, accident, and arson scene investigation, and in SWAT ̶ Hover ability is very beneficial ̶ Some systems are relatively quiet, providing stealth, and can “perch” ̶ Up to 50-min endurance was tested/verified – winds are not a limiting factor (flying in winds up to 30 mph) ̶ In winds, maintain commanded flight profiles better than fixed wing aircraft 18 Lessons Learned, cont’d • Essential capabilities for effective, high-use operations: ̶ Integrated EO and IR sensors on a stabilized, gimbaled platform • SAR aided by ability to switch between two modes to validate Targets of Interest (TOI) • Dual sensors are valuable in urban scenarios where shadows are prevalent ̶ Geo-referenced EO and IR full motion video • Needed for chain of custody and TOI location accuracy • Collision avoidance: ̶ For some systems, the best way to avoid oncoming traffic may be to initiate immediate landing – but climb and descend speeds may not be sufficient to avoid collision • Other findings: ̶ Quiet systems developed by DOD may need audible augmentation during SAR ̶ The fuel cell SUAS we tested is a significant new capability: > 8 hr endurance • Note to potential users: It requires > 12 min for warm-up prior to launch 19 Future Outlook Cycle 1, FY2012-14 • 2012 – Range selection; advocacy – Define program scope and set key partnerships – RFI; Test Plan; contracting • Stand up: – Processes to work with manufacturers, create and disseminate reports – Liaison to DHS privacy working group • Conduct 19 flight test weeks • Analyze and disseminate results from Cycle 1 testing Cycle 2, FY2015-16 • New RFI; new Test Plan • Expanded test scope (goals): – Fire/HAZMAT/disaster, SAR response – Specialized SUAS sensors – Larger, more complex operational scenarios – Counter-spoofing and antijamming capabilities – Airworthiness • Severe storm response pilot – RAMPS new start: Maritime testing, USCG RDC-led collaboration – Transition Plan for future funding and management structure 20 Project Office, Web Links RAPS Project Support Officer: – Mr. Kevin Spence: (202) 254-2235 kevin.spence@associates.hq.dhs.gov RAPS and related Web Links: – http://www.firstresponder.gov is a public-access DHS S&T website – Government employees and government-sponsored stakeholders interested in RAPS may request access to the RAPS Test Reports via http://www.firstresponder.gov, which is the gateway to access S&T’s First Responder Communities of Practice site, https://communities.firstresponder.gov, which is the gateway to the RAPS Community of Practice site. Access is controlled by DHS S&T and the RAPS Program Manager. – RAPS Request for information (RFI), released September 24, 2012: https://www.fbo.gov/spg/DHS/OCPO/DHS-OCPO/DHS13-01/listing.html • RAPS Privacy Impact Assessment (PIA), approved Nov. 16, 2012, was the first such document addressing unmanned aircraft ever published – anywhere in the world: http://www.dhs.gov/sites/default/files/publications/privacy/PIAs/privacy_pia_st_ raps_nov2012.pdf 21 LESSONS LEARNED • No one platform performs well in all scenarios • Some fixed winged SUAS may need operating areas > 200 ft radius – Launch and recovery zones – Deep stall landings affected by winds • Fixed wing aircraft are very good in search and rescue and fire monitoring • Rotary winged platforms perform well in crime, accident, and arson scene investigation and in police SWAT applications – Hover ability is very beneficial – Some systems are relatively quiet, providing stealth, and can “perch” at specific locations • Quiet systems developed by the Department of Defense may need audible augmentation during search and rescue • Fuel cells provide endurance > 8 hours but require > 12 minutes to warm up prior to launch 23 LESSONS LEARNED (cont’d) • Integrated EO and IR sensors on a gimbaled platform is essential – Search and rescue scenarios are aided by ability to switch between two modes to validate targets of interest – Dual sensors are valuable in urban scenarios where shadows are prevalent • Geo-referencing EO and IR full motion video is essential – Needed for chain of custody and target of interest location accuracy • For some systems, the best way to avoid traffic may be to initiate immediate landing – Climb and descent speeds may not be sufficient to avoid collision • Rotary winged aircraft are nearing the 30-minute endurance level – Winds are not a limiting factor (fly in winds up to 30 mph) – Can maintain commanded flight profiles 24 RAPS STEERING GROUP Dr. John Appleby, Chair DHS S&T HSARPA Mr. Bob Griffin, Director DHS S&T First Responder Group Mr. Jonathan Cantor DHS Chief Privacy Officer (Act.) Ms. Tamara Kessler, Chief (Act.) DHS Office for Civil Rights and Civil Liberties Mr. John Priddy, Director DHS Customs and Border Protection (CBP)/ Air Operations Capt Doug Nash, Chief DHS U.S. Coast Guard/ Office of Aviation Forces Mr. Chris Vaughan DHS Federal Emergency Management Admin./ Geospatial Management Office Mr. Jim Williams, Director Federal Aviation Administration (FAA)/ UAS Integration Office Mr. David Morton FAA/ UAS Integration Office, Aviation Safety Inspector Mr. Steve Pansky FAA/ UAS Integration Office, Senior ATC Analyst Dr. Steve McKeever Oklahoma State Univ./ VP for Science &Technol. Transfer; UML/ Executive Director Mr. Eric Meyn, Director University Multispectral Laboratories (UML)/ Unmanned Systems Division Chief Robert Doke Oklahoma State Fire Marshall Chief Jon Hansen Director, Oklahoma Council On Firefighter Training (COFT) LTC Jon Greenhaw Oklahoma National Guard Mr. Mike O’Shea Department of Justice/ Office of Justice Programs Cmdr Bob Osborne (ret.) Los Angeles County Sheriff’s Department Chief Donald Shinnamon, Sr. (ret.) Public Safety Aviation Consultant Mr. Andy Lacher MITRE Corporation/ UAS Integration Research Strategist 25 PRIVACY http://www.gigapixel.com/image/gigapan-canucks-g7.html 26