Autonomous Landing Hazard Avoidance Technology (ALHAT) Lidar Sensor Performance in Closed- Loop Flight Testing of the Morpheus Rocket-Propelled Lander to a Lunar-Like Hazard Field V. Eric Roback (presenting), Diego F. Pierrottet, Farzin Amzajerdian, Bruce W. Barnes, Alexander E. Bulyshev, Glenn D. Hines, Larry B. Petway, Paul F. Brewster, and Kevin S. Kempton NASA-Langley Research Center, Hampton, VA AIAA SciTech 2015, January 5 – 9, 2015 Gaylord Palms Hotel and Convention Center, Kissimmee, FL ALHAT / Morpheus Lidars: SciTech 2015 Page1 1/5/2015 Planetary Landing: the Problem Autonomous Landing Hazard Avoidance Technology (ALHAT) • Existing state-of-art Apollo 15 – Optical photos from orbit (dependent on favorable solar illumination) – Laser mapping from orbit – Low resolution hazard detection – Not real-time – Restricts landing to un-challenging lighting & terrain Brady, T., and S. Paschall, The Challenge of Safe Lunar Landing, Proc. of IEEE Aerospace Conference, Big Sky, MT, March 6 – 13, 2010, pp. 1 – 14. ALHAT / Morpheus Lidars: SciTech 2015 Page2 1/5/2015 ALHAT Solution Autonomous Landing Hazard Avoidance Technology (ALHAT) • GN&C & sensing system – Crewed or robotic – Safe – Precise (30m,1σ) – Any ambient lighting (use lidars) – Real-time DEM’s • System goals – Detect 30cm hazards @1km – 1 cm/s velocity Hazard Detection precision & Precision – 20 cm range Guidance precision (1km to 100m) ALHAT / Morpheus Lidars: SciTech 2015 Page3 1/5/2015 Lidars Installed on Morpheus Navigation Doppler Flash Lidar EAluetcontroomnoiucss L anding FHlaazsahrd LAivdoaidra Snceen Tseocrh nHoeloagdy ((AFLLHSAHT)) Lidar (NDL) Chassis Box (LEB) Mounted to HDS 2-axis Gimbal Laser Altimeter NDL Optical (LA) Head ALHAT / Morpheus Lidars: SciTech 2015 Page4 1/5/2015 Field Test Plan Autonomous Landing Hazard Avoidance Technology (ALHAT) 5 flights in spring 2014: 3 open-loop & NASA-Kennedy 2 closed-loop (1 at night ~ 10pm) Shuttle Landing Facility (SLF) 100 m 100 m ALHAT / Morpheus Lidars: SciTech 2015 Page5 1/5/2015 Morpheus on Approach Autonomous Landing Hazard Avoidance Technology (ALHAT) Flash Lidar Sensor Head KSC Shuttle Landing Facility Hazard Field (100m X 100m) Runway 15 Approach Lights ALHAT / Morpheus Lidars: SciTech 2015 Page6 1/5/2015 Flash Lidar Specs Autonomous Landing Hazard Avoidance Technology (ALHAT) • Max range: 1.35km Sensor Head • # pixels: 128 x 128 = 16,384 (FLSH) • Range precision: 8 cm (1σ) – Allows 30cm hazard Goal detection@1km Met Electronics Box • Size: (LEB) – FLSH: 11x13.5x13.25 inches – LEB: 9.5x14.2x13 inches • Weight: – FLSH: *36 lbs – LEB: *36 lbs • Power: *450 Watts * Dominated by terrestrial cooling system ALHAT / Morpheus Lidars: SciTech 2015 Page7 1/5/2015 Flash Lidar Principles of Operation Autonomous Landing Hazard Avoidance Technology (ALHAT) Target 8ns pulse width 1° wide area “freezes” target motion beam • Round-trip time of flight – Range = speed of light x round-trip time of flight / 2 • 3-D images generated in real-time – One image per laser shot – 128 x 128 pixels (16,384) per image – 20 images/sec output ALHAT / Morpheus Lidars: SciTech 2015 Page8 1/5/2015 Flash Lidar Flight Data Autonomous Landing Hazard Avoidance Technology (ALHAT) Rock 1 Rock 2 Rock 1 (30cm) Rock 2 Safe (28cm) Site Hazard Detection Goals Met Mission Elapsed Time (MET) = 45.641564 sec MET = 46.036214 sec FF11 (Day) FF14 (Night ~ 10pm) Rock 1 Rock 1 Rock 2 Rock 2 Range ~ 425m Range ~ 425m ALHAT / Morpheus Lidars: SciTech 2015 Page9 1/5/2015 Rocket Plume Heat Effects on Flash Lidar (scintillation) Autonomous Landing Hazard Avoidance Technology (ALHAT) FF11 (no issue) - FF12 (scintillation issues) - 3400 3400 MET = 44.141766 sec MET = 43.634655 sec - 3000 nI - 3000 nI t t e e n n s s ti ti - 2600 y - 2600 y ( ( c c o - o u u n n - 2200 st - 2200 st ) ) - 1800 - 1800 Apply wind restrictions for future flights Safe Scintillation Safe Site Site Smearing ALHAT / Morpheus Lidars: SciTech 2015 Page10 1/5/2015