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GN and C Subsystem Concept for Safe Precision Landing of the Proposed Lunar MARE Robotic Science MissionThe Lunar MARE (Moon Age and Regolith Explorer) Discovery Mission concept targets delivery of a science payload to the lunar surface for sample collection and dating. The mission science is within a 100-meter radius region of smooth lunar maria terrain near Aristarchus crater. The location has several small, sharp craters and rocks that present landing hazards to the spacecraft. For successful delivery of the science payload to the surface, the vehicle Guidance, Navigation and Control (GN&C) subsystem requires safe and precise landing capability, so design infuses the NASA Autonomous precision Landing and Hazard Avoidance Technology (ALHAT) and a gimbaled, throttleable LOX/LCH4 main engine. The ALHAT system implemented for Lunar MARE is a specialization of prototype technologies in work within NASA for the past two decades, including a passive optical Terrain Relative Navigation (TRN) sensor, a Navigation Doppler Lidar (NDL) velocity and range sensor, and a Lidar-based Hazard Detection (HD) sensor. The landing descent profile is from a retrograde orbit over lighted terrain with landing near lunar dawn. The GN&C subsystem with ALHAT capabilities will deliver the science payload to the lunar surface within a 20-meter landing ellipse of the target location and at a site having greater than 99% safety probability, which minimizes risk to safe landing and delivery of the MARE science payload to the intended terrain region.
Document ID
20170009195
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
External Source(s)
Authors
Carson, John M., III
(NASA Johnson Space Center Houston, TX, United States)
Johnson, Andrew E.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Anderson, F. Scott
(Southwest Research Inst. San Antonio, TX, United States)
Condon, Gerald L.
(NASA Johnson Space Center Houston, TX, United States)
Nguyen, Louis H.
(NASA Johnson Space Center Houston, TX, United States)
Olansen, Jon B.
(NASA Johnson Space Center Houston, TX, United States)
Devolites, Jennifer L.
(NASA Johnson Space Center Houston, TX, United States)
Harris, William J.
(NASA Johnson Space Center Houston, TX, United States)
Hines, Glenn D.
(NASA Langley Research Center Hampton, VA, United States)
Lee, David E.
(NASA Johnson Space Center Houston, TX, United States)
Amzajerdian, Farzin
(NASA Langley Research Center Hampton, VA, United States)
Trawny, Nikolas
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Lawrence, Samuel
(Arizona State Univ. Tempe, AZ, United States)
Huertas, Andres
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Johnson, Wyatt
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
September 29, 2017
Publication Date
January 4, 2016
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
JSC-CN-34826
AIAA 2016-0100
Report Number: JSC-CN-34826
Report Number: AIAA 2016-0100
Meeting Information
Meeting: AIAA Guidance, Navigation, and Control Conference
Location: San Diego, CA
Country: United States
Start Date: January 4, 2016
End Date: January 8, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNX09CB10C
CONTRACT_GRANT: NNN06AA01C
TASK: NN07AA19T
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
MARE (Moon Age and Regolith Explorer)
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