Ground Based Sense and Avoid (GBSAA) 101 Overview

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Aerospace Management Systems Division Ground Based Sense and Avoid (GBSAA) 101 Overview Roger Francis, GBSAA Team Lead The MITRE Corporation CNS/ATM Conference 2011 2011 The MITRE Corporation Distribution Statement A: Approved for public release: 11-2488 and 66ABW-2011-0694. Distribution Unlimited

Outline Background Bed-down Locations Desired Outcome Pieces of the Puzzle Architecture Tools Demonstrations ATC enablers Conclusions 2

Background Unmanned Aircraft Systems (UAS)/Remotely Piloted Aircraft (RPA) have proven themselves in combat situations But flying RPAs in the U.S. National Airspace System (NAS) is still a challenge Two means are available: Fly in Restricted airspace or implement a Temporary Flight Restriction (TFR) during UAS operations Fly under a Certificate of Authorization or Waiver (COA), which specifies means to safely separate and avoid traffic conflicts Ground observers Chase planes Both FAA and DoD seek a more permanent solution Airborne sense and avoid capabilities are still years away But ground-based sense and avoid (GBSAA) could well work now

NextGen & RPA Challenges Public Law #108-176 (2003), The Vision 100 Century of Aviation Reauthorization Act Mandate for the design and deployment of an air transportation system to accommodate a wide range of aircraft operations, including airlines, air taxis, helicopters, general aviation, and unmanned aerial vehicles to meet the nation s needs by 2025 (i.e.-nextgen). DoD NextGen Lead Service Memo (28 Dec 07)- OPR-Gordon England- Dep Sec Def NextGen also addresses unique DoD requirements These include Homeland Defense policies and programs, special use airspace for training and ranges, employment of unmanned aircraft systems, and surveillance of the air and maritime domains. DoT -IG Report (21 Apr 10) OPR-Honorable Calvin Scovel III Need Sense & Avoid (SAA) to realize potential for File & Fly GBSAA - near term solution the evolving use of UAS technology has become an important issue for FAA, DOD, DHS and other agencies. However, there are no established cross-agency requirements for UAS or a clear understanding of how they will be used in a NextGen environment. 4

USAF Ground Based Sense and Avoid Locations * UAS/UA aka Remotely Piloted Aircraft (RPA) 5

Airspace Integration Overview - DoD UAS Airspace Access Planned DoD UAS bed-down by 2013 requires: 113 CONUS locations 1.1M UAS flight hours (vs 3.3M manned aircraft hours) - Required for initial & continuation training - Small UAS (Group 1) will fly 77% of 1.1M hours in the 2013 timeframe 91% of the airspace UAS will need to use Class E & G airspace - Majority of non-cooperative traffic also operate in Class E & G - Presents the highest accident potential 2008 2013 Army Air Force Navy Marines SOCOM State ID d but Post TBD Army Air Force Navy Marines SOCOM State ID d but Post TBD

UAS Airspace Integration Outcome Enable routine unmanned aircraft operations in nonsegregated civil airspace To satisfy Military, Federal, and public-interest mission and training needs While maintaining current level of civil airspace safety Without adverse impacts on civil aviation operations and efficiencies While also enabling growth of commercial UAS applications 7

Considerations Solution needs to include: Maximizing use of existing resources Gap filler capabilities/technologies Operational procedures development (Major variable) Key factors to ensure safe RPA operations Performing comprehensive safety analyses Defining and implementing operational procedures Conclusively demonstrating a positive impact upon the overall safety of the NAS DoD GBSAA must prove that the GBSAA system provides safe separation of aircraft 8

Pieces of the GBSAA Puzzle FAA Workshop May 2009

GBSAA Architecture Airborne Objects / Targets Non-cooperative Aircraft UAS Class E & G Airspace Avoidance Maneuvering Radars Display Tracker Ground Observer Ground Control System (GCS) Air Traffic Controller (ATC) 10

CRADA is One Tool Cooperative Research and Development Agreement (CRADA) Formalized arrangement - government and collaborators cooperate to develop & use shared resources No funds are exchanged Participants fund own contribution to the shared asset Modifies assets as needed for exercises using the shared asset Time limited; typically two-year duration but can be extended w/ agreement by both participants 11

Raytheon & ESC/HBAI CRADA Leverage existing ATC systems to improve RPA access to NAS Optimize tracker for GBSAA Dynamic Protection Zone (DPZ) to provide pilot with traffic information to effect self-separation threshold Leverage future ASR-11 capability (PSR Altitude Estimation) Reduce clutter, e.g. wind turbines, terrain Improve Probability of detection (Pd) and positional accuracy of non-cooperative targets Provide more options for maneuvering around traffic Approved for Public Release #11-2488 Altitude on non-cooperative air vehicles 12

Compile data from radar sensors that: Airspace Characterization Includes both non-cooperative (search-only) and beacon targets Has been associated into tracks Determine traffic patterns such as: 3-dimensional distributions, with separate altitude and horizontal distributions Velocity and climb/descend rate distributions Time distributions such as day-of-the-week and hour-of-the-day Correlations between altitude and velocity, altitude and hits, etc. Compare the results from the various sensors to determine: Which targets are detected and not detected by multiple sensors Which targets are likely to be noise and not real airborne targets Which sensors are most viable for a ground based sense and avoid (GBSAA) system, complementing each others strengths and weaknesses Support the design for a GBSAA that will: Minimize exposure to other air traffic Enable safe Remotely Piloted Aircraft (RPA) operations 13

M&S Track Initiation Analysis Evaluate time required to see (initiate track) on a pop-up intruder Relies on Airspace PD Coverage Modeling Model considers: Random intruder pop-ups in Airspace PD of Radar(s) at given <Lat, Lon, Alt> Radar asynchronous update rates Tracking system logic (m of n criteria) Results Distribution of track initiation times Where can we fly in the airspace? Minimum altitude limits for sufficient time to initiate track on intruders UAS Intruder Earth UAS Bottom of Radar Coverage Fly high enough above the bottom of the coverage to allow sufficient time to detect and track targets Safe Altitude Limit Avoidance Maneuver Buffer Buffer for Track Initiation Intruder 14

Two Approaches for GBSAA Modified Zero Conflict Airspace (ZCA) Test site is Cannon AFB Geographic Display Only RPA or civil aircraft in statically defined airspace at same time Near term improvement to COA Dynamic Protection Zone (DPZ) Test site is Gray Butte Airfield Pilot centric display RPA flies with civil aircraft in non-segregated airspace 15

Army Zero Conflict Alert Concept Army Zero Conflict Airspace Concepts: Airspace Volumes of Interest (AVOIs) can be used to support the constructs of Zero Conflict Airspace (ZCA). Diagram of Army requirements for GBSAA. Our capabilities will provide for alerts based on these 3-D elements. Zero Conflict Airspace 16

Dynamic Protection Zone 0 330 30 Collaboration with USAF ESC & MITRE DPZ shape and separation thresholds studied. STARS constructs a DPZ around the RPA so any trajectory penetration will provide an intrusion alert in a configurable time frame Shape evolved from kidney-bean alert zone to the current shape. 270 300 240 5000 10000 15000 60 120 Erroneous DPZ Shape Correct DPZ Shape Example scenario of RPA and another 20000 target on a collision 90 course. 210 150 180 Self Separation Threshold Direction of flight Conflict Avoidance Threshold Min & Max Altitude RPA Evolution of Display Capabilities Direction of flight STARS GBSAA DPZ Self Separation Threshold Green circle, of radius ("B") represents distance the track can travel in an adaptable time (e.g. 60 seconds) at its current ground-speed. The distance ("A") between the track and the center of the circle will be a percentage of the circle's radius. Direction of Flight Collision Avoidance Threshold Yellow circle, of radius ("D") represents distance (i.e. 30 sec) track can travel at its current ground-speed. The distance ("C") between the track and the center of the circle would be a percentage of the circle's radius. Approved for Public Release #11-2488 Collision Volume For the RPA, the fused-track "filled blue circle" will be used. Represents an area that 'covers' the location of the aircraft with an 80% confidence level.

Gray Butte Concept Demonstration Current Gray Butte operations require chase aircraft Proof of Concept will be used to demonstrate the viability of GBSAA using the Dynamic Protection Zone (DPZ) approach ASR-11 at Edwards will be used as well as BORON longrange radar Self separation will be accomplished using DPZ Raytheon CRADA leverages STARS LITE fusion tracker with DPZ development with alerting for RPA Pilot Airspace characterization, NMAC probability, P d, M&S, etc. all part of overall safety case Proof of Concept activities will be used to develop Program of Record requirements Approved for Public Release #11-2488

ATC Enablers for GBSAA Advanced Signal Data Processor Replaces obsolete SDP FAA/DoD fielding underway for all ASR- 11s Raytheon Concurrent Beam Processing (CBP) for UK ATC radars w/ ASDP Terminal ATC radars well-placed throughout the NAS to support GBSAA mission needs STARS LITE Smaller scale STARS workstation Fusion tracker Integrates up to 3 radar feeds Installed @ FAA contract towers Army/USAF planning to deploy @ remote towers (ASDP) ASR-11 w/ ASDP ASR-9/-11 CONUS Airspace Coverage (5k ft AGL) Approved for Public Release #11-2488 19

ATC Radars Currently Measure only Range and Azimuth Impact of the Tracker d 1. A tracker takes sequential detections and connects them into a track that represents a single object moving through the airspace 2. Mosaic Tracker works with data from only one radar at a time 3. Fusion Trackers combine the data from multiple radars and combine them into a single track 4. Fused detections from 2 radars has P d ~ 99.75% 5. Track Initiation Criteria is important 1. Range precision is 1/64 nmi or greater 2. Azimuth precision fixed ~2 degrees Location uncertainty increases with Range 3. Probability of Detection (P d ) for a single modern terminal radar ~ 95% Depends on the tuning/filtering 4. Weight the degree of reliance you can assign each detection depending on distance of radar from the a/c d Exaggerated Azimuth Resolutions

Conclusions Airspace characterization tool set developed Input: AREPS Output, Range vs. Altitude Slices at all Azimuths Output: P d as a function of <Lat, Lon, Alt> Explore airspace radar coverage Combined coverage from multiple radars Concurrent beam processing Track Initiation model developed Dependent on P d model (discussed above) Model validated and verified Track Initiation Time Simulation Conduct simulations appropriate for determining statistically significant results Initial Results for Grand Forks AFB (test case) and Edwards AFB AREPS output for Cannon AFB available Safety case development has started with AFSC Approved for Public Release #11-2488 21

Questions? Approved for Public Release #11-2488

GBSAA Contacts Hanscom AFB Comm Prefix 781-377-XXXX Hanscom AFB DSN 478-XXXX Capt Robert Walker 7791 Mr Kevin Carey 8194 Mr Roger Francis 9127 Mr Bill Hershey 937-623-4365 Mr Chris Jella 703-463-8237 Mr Kyle Noth 7594 Ms Bette Winer 9044 23

Backup Slides 24

Target Altitude Estimation Tests have been conducted at Stockton (2005), FAATC (2007), and Travis AFB (2008) to establish the advantages of the concurrent beams configuration versus the standard switched beam configuration US Patent number 4,961,075 Two and one-half dimensional radar system, Harold R Ward Altitude Upper/Lower Beam Target Amplitude Ratio Estimated Altitude Short Pulse Long Pulse Antenna Gain Estimated Altitude based on Upper/Lower Beam Target Amplitude Ratio Approved for Public Release: 10-1359. Distribution Unlimited

GBSAA CRADA Background ESC/HBA GBSAA CRADA Signed by Raytheon (Collaborator) Leverages existing ATC systems to improve RPA access to NAS Demonstrate fused ASR-9/-11 (ATC) show same tracks as Sentinel (AD) Use Dynamic Protection Zone (DPZ) to improve GBSAA effectiveness Leverages future ASR-11 capability (PSR Altitude Estimation) to Reduce clutter, e.g. wind turbines Improve Probability of detection (Pd) and positional accuracy of noncooperative targets Gov t SMEs proactively engaged w/ Raytheon technical staff Radar data collected @ Edwards AFB 26

GBSAA CRADA Issue: Terminal ATC radars (ASR-9/-11) can detect non-cooperative targets to support GBSAA. However, routine velocity filtering in ATC tracker discards reports for slowmoving/non-cooperative aircraft. Proposal: 2-Tracks Track I (Clutter Control/Tracking) Develop appropriate radar tracker configuration (using STARS LITE) to support GBSAA mission @ Gray Butte & Cannon AFB Use STARS LITE tracker for detecting objects flying below the usual ATC Velocity filter Use DPZ SW with STARS LITE to allow UAS operations in non segregated airspace Track 2 (Altitude Estimation) Use DASR w/ ASDP to validate concurrent beam processing (future DASR enhancement) to provide improved detection and positional accuracy (X,Y,Z) of non-cooperative targets Approved for Public Release #11-2488 ATC Display 8 4 DPZ UAS Pilot/Observer Display STARS LITE Alt Estimation

GBSAA CRADA Operational View for Track 1 Terminal ATC RADAR (Recorded) Plots Tracker for GBSAA (STARS LITE) GBSAA- Optimized Tracks & Plots UAS GCS - GBSAA RPA Observer's Display Tracks ATC- Optimized Tracks & Plots ATC Display Plots Tracker for ATC Automation TRACKS TRACON - ATM Approved for Public Release #11-2488

ASR-10SS / DASR with ASDP (Test Configuration) Hi Beam Low Beam Wx Channel Feeds New Software Build installed on existing SCDI workstations Target High Beam and Weather input cables swapped over Beam Switch / Combiner bypassed (at rear of unit) FAA/DoD ordered ASDP retrofit kits for fielded systems Stand-alone Enhanced Tracker (in external PC chassis) Used with permission SDP chassis swapped out for ASDP chassis Raytheon awarded contract to develop Concurrent Beam Processing for UK ATC radars Page 29