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Absolute stability analysis of attitude control systems for large boosters.A method for performing an absolute stability analysis of attitude control systems for large launch vehicles is presented. Absolute stability of these systems is shown to be of a limited extent. The regions of absolute stability are computed by using a quadratic Liapunov function. The function is chosen to provide additional information about the exponential property of absolute stability. A system model is used to illustrate the method.
Document ID
19720032809
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Siljak, D. D. (Santa Clara, University Santa Clara, Calif., United States)
Seltzer, S. M. (NASA Marshall Space Flight Center Astrionics Laboratory, Huntsville, Ala., United States)
Date Acquired
August 6, 2013
Publication Date
January 1, 1971
Subject Category
Space Vehicles
Meeting Information
Meeting: Symposium on Automatic Control in Space
Location: Dubrovnik
Country: Yugoslavia
Start Date: September 6, 1971
End Date: September 10, 1971
Accession Number
72A16475
Funding Number(s)
CONTRACT_GRANT: NGR-05-017-101
Distribution Limits
Public
Copyright
Other

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