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Optimal Terminal Descent Guidance Logic to Achieve a Soft Lunar TouchdownAltair Lunar Lander is the linchpin in the Constellation Program for human return to the Moon. In the 2010design reference mission, Altair is to be delivered to low Earth orbit by the Ares V heavy lift launch vehicle, and after subsequent docking with Orion in LEO, the Altair/Orion stack is delivered through trans-lunar injection (TLI). The Altair/Orion stack separates from the Ares V Earth departure stage shortly after TLI and continues the flight to the Moon as a single stack. Fig. 1 depicts one version of the Altair lunar lander.
Document ID
20110020603
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Lee, Allan Y.
(California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 25, 2013
Publication Date
August 8, 2011
Subject Category
Space Transportation And Safety
Meeting Information
Meeting: AIAA Guidance, Navigation, and Control Conference
Location: Portland, OR
Country: United States
Start Date: August 8, 2011
End Date: August 11, 2011
Distribution Limits
Public
Copyright
Other
Keywords
Landing
optimal control
Soft touchdown
Lunar landing

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