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Preparation and Integration of ALHAT Precision Landing Technology for Morpheus Flight TestingThe Autonomous precision Landing and Hazard Avoidance Technology (ALHAT) project has developed a suite of prototype sensors for enabling autonomous and safe precision land- ing of robotic or crewed vehicles on solid solar bodies under varying terrain lighting condi- tions. The sensors include a Lidar-based Hazard Detection System (HDS), a multipurpose Navigation Doppler Lidar (NDL), and a long-range Laser Altimeter (LAlt). Preparation for terrestrial ight testing of ALHAT onboard the Morpheus free- ying, rocket-propelled ight test vehicle has been in progress since 2012, with ight tests over a lunar-like ter- rain eld occurring in Spring 2014. Signi cant work e orts within both the ALHAT and Morpheus projects has been required in the preparation of the sensors, vehicle, and test facilities for interfacing, integrating and verifying overall system performance to ensure readiness for ight testing. The ALHAT sensors have undergone numerous stand-alone sensor tests, simulations, and calibrations, along with integrated-system tests in special- ized gantries, trucks, helicopters and xed-wing aircraft. A lunar-like terrain environment was constructed for ALHAT system testing during Morpheus ights, and vibration and thermal testing of the ALHAT sensors was performed based on Morpheus ights prior to ALHAT integration. High- delity simulations were implemented to gain insight into integrated ALHAT sensors and Morpheus GN&C system performance, and command and telemetry interfacing and functional testing was conducted once the ALHAT sensors and electronics were integrated onto Morpheus. This paper captures some of the details and lessons learned in the planning, preparation and integration of the individual ALHAT sen- sors, the vehicle, and the test environment that led up to the joint ight tests.
Document ID
20140009928
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Carson, John M., III
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Robertson, Edward A.
(NASA Johnson Space Center Houston, TX, United States)
Pierrottet, Diego F.
(Coherent Applications, Inc. Hampton, VA, United States)
Roback, Vincent E.
(NASA Langley Research Center Hampton, VA, United States)
Trawny, Nikolas
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Devolites, Jennifer L.
(NASA Johnson Space Center Houston, TX, United States)
Hart, Jeremy J.
(NASA Johnson Space Center Houston, TX, United States)
Estes, Jay N.
(NASA Johnson Space Center Houston, TX, United States)
Gaddis, Gregory S.
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Date Acquired
July 21, 2014
Publication Date
August 4, 2014
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
JSC-CN-31442
Meeting Information
Meeting: AIAA Space 2014 Conference
Location: San Diego, CA
Country: United States
Start Date: August 4, 2014
End Date: August 7, 2014
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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