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Approach-Phase Precision Landing with Hazard Relative Navigation: Terrestrial Test Campaign Results of the Morpheus/ALHAT ProjectThe Morpheus Project began in late 2009 as an ambitious e ort code-named Project M to integrate three ongoing multi-center NASA technology developments: humanoid robotics, liquid oxygen/liquid methane (LOX/LCH4) propulsion and Autonomous Precision Landing and Hazard Avoidance Technology (ALHAT) into a single engineering demonstration mission to be own to the Moon by 2013. The humanoid robot e ort was redirected to a deploy- ment of Robonaut 2 on the International Space Station in February of 2011 while Morpheus continued as a terrestrial eld test project integrating the existing ALHAT Project's tech- nologies into a sub-orbital ight system using the world's rst LOX/LCH4 main propulsion and reaction control system fed from the same blowdown tanks. A series of 33 tethered tests with the Morpheus 1.0 vehicle and Morpheus 1.5 vehicle were conducted from April 2011 - December 2013 before successful, sustained free ights with the primary Vertical Testbed (VTB) navigation con guration began with Free Flight 3 on December 10, 2013. Over the course of the following 12 free ights and 3 tethered ights, components of the ALHAT navigation system were integrated into the Morpheus vehicle, operations, and ight control loop. The ALHAT navigation system was integrated and run concurrently with the VTB navigation system as a reference and fail-safe option in ight (see touchdown position esti- mate comparisons in Fig. 1). Flight testing completed with Free Flight 15 on December 15, 2014 with a completely autonomous Hazard Detection and Avoidance (HDA), integration of surface relative and Hazard Relative Navigation (HRN) measurements into the onboard dual-state inertial estimator Kalman lter software, and landing within 2 meters of the VTB GPS-based navigation solution at the safe landing site target. This paper describes the Mor- pheus joint VTB/ALHAT navigation architecture, the sensors utilized during the terrestrial ight campaign, issues resolved during testing, and the navigation results from the ight tests.
Document ID
20170009198
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Crain, Timothy P.
(Intuitive Machines Houston, TX, United States)
Bishop, Robert H.
(University of South Florida Tampa, FL, United States)
Carson, John M., III
(NASA Johnson Space Center Houston, TX, United States)
Trawny, Nikolas
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Hanak, Chad
(NASA Johnson Space Center Houston, TX, United States)
Sullivan, Jacob
(NASA Johnson Space Center Houston, TX, United States)
Christian, John
(West Virginia Univ. Morgantown, WV, United States)
DeMars, Kyle
(Missouri Univ. of Science and Technology Rolla, MO, United States)
Campbell, Tom
(Intuitive Machines Houston, TX, United States)
Getchius, Joel
(Intuitive Machines Houston, TX, United States)
Date Acquired
September 29, 2017
Publication Date
January 4, 2016
Subject Category
Spacecraft Instrumentation And Astrionics
Space Transportation And Safety
Report/Patent Number
JSC-CN-35003
Report Number: JSC-CN-35003
Meeting Information
Meeting: AIAA SciTech 2016
Location: San Diego, CA
Country: United States
Start Date: January 4, 2016
End Date: January 6, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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