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A manually retargeted automatic descent and landing system for LM.Manual steering problem and function of lunar module /LM/ manual hybrid guidance system, with automatic guidance system produced trajectory
Document ID
19670060447
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Klumpp, A. R.
Date Acquired
August 3, 2013
Publication Date
September 1, 1967
Subject Category
Space Vehicles
Accession Number
67A39176
Funding Number(s)
CONTRACT_GRANT: NAS9-4065
Distribution Limits
Public
Copyright
Other
Keywords
MANUAL CONTROL
TRAJECTORY CONTROL
APPROACH CONTROL
GUIDANCE (MOTION)
LUNAR LANDING MODULE

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