Application Of High Moment-Producing Techniques For Control Of A Manned Space Vehicle
Item
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Title
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Application Of High Moment-Producing Techniques For Control Of A Manned Space Vehicle
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Date
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1964
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Index Abstract
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Coming Soon
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Photo Quality
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Not Needed
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Report Number
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FDL TDR 64-32 Final Report
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Creator
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None Given
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Corporate Author
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Bendix Corp Southfield Mich
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Laboratory
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AF Flight Dynamics Laboratory
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Extent
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410
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Identifier
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AD0439202
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Access Rights
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OTS
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Distribution Classification
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1
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Contract
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AF 33(657)-10998
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DoD Project
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8225
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DoD Task
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822503
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DTIC Record Exists
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No
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Distribution Change Authority Correspondence
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None
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Abstract
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The application is studied of high moment-producing techniques for the attitude control of manned space vehicles which perform orbital transfer, rendezvous, and lifting re-entry maneuvers. The specific accomplishments were: (a) establishment of control system, subsystem and component requirements for critical vehicle flight phases, and (b) analysis of promising techniques for performing the flight control functions required during the various maneuvers. A hypothetical vehicle was selected and its space mission was analyzed to determine the attitude control requirements. The rendezvous and re-entry maneuvers were found to be especially demanding on the attitude control system.
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Report Availability
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Full text available
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Date Issued
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1964-03
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Provenance
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Lockheed Martin Missiles & Fire Control
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Type
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report
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Format
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1 online resource