Application Of High Moment-Producing Techniques For Control Of A Manned Space Vehicle

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Report Number: FDL TDR 64-32 Summary Final Report
Author(s): None Given
Corporate Author(s): Bendix Corp Southfield Mich
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-03
Pages: 64
Contract: AF 33(657)-10998
DoD Project: 8225
DoD Task: 822503
Identifier: AD0439201

Abstract:
High moment-producing techniques are applied to the attitude control of manned space vehicles which perform orbital transfer, rendezvous, and lifting re-entry maneuvers. The specific accomplishments were: (1) establishment of control system, subsystem and component requirements for critical vehicle flight phases, and (2) analysis of promising techniques for performing the flight control functions required during the various maneuvers.

Provenance: Lockheed Martin Missiles & Fire Control

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