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Effect of observation uncertainties on the performance of a predictive guidance system used for descent from lunar orbit.Navigation and control sensor error effect on guidance system performance for lunar landing vehicles
Document ID
19650027988
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Taylor, R. L.
Date Acquired
August 2, 2013
Publication Date
January 1, 1964
Subject Category
Navigation
Accession Number
65A10692
Funding Number(s)
CONTRACT_GRANT: NASW-460
Distribution Limits
Public
Copyright
Other
Keywords
TERMINAL GUIDANCE
SPACECRAFT GUIDANCE
LUNAR LANDING
DESCENT TRAJECTORY
GUIDANCE SENSOR

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IDRelationTitle19650027979Collected WorksAmerican institute of aeronautics and astronautics, and nasa, manned space flight meeting, 3rd, houston, tex., november 4-6, 1964, technical papers /aiaa publication cp-10/.19650027979Collected WorksAmerican institute of aeronautics and astronautics, and nasa, manned space flight meeting, 3rd, houston, tex., november 4-6, 1964, technical papers /aiaa publication cp-10/.
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