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

Item

Title
Application Of High Moment-Producing Techniques For Control Of A Manned Space Vehicle
Date
1964
Index Abstract
Coming Soon
Photo Quality
Not Needed
Report Number
FDL TDR 64-32 Final Report
Creator
None Given
Corporate Author
Bendix Corp Southfield Mich
Laboratory
AF Flight Dynamics Laboratory
Extent
410
Identifier
AD0439202
Access Rights
OTS
Distribution Classification
1
Contract
AF 33(657)-10998
DoD Project
8225
DoD Task
822503
DTIC Record Exists
No
Distribution Change Authority Correspondence
None
Abstract
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.
Report Availability
Full text available
Date Issued
1964-03
Provenance
Lockheed Martin Missiles & Fire Control
Type
report
Format
1 online resource

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