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Application of C-minimax optimal control theory to flight control problems.Spacecraft and large launch vehicle nonoptimal /suboptimal/ controllers evaluated with Chebyshev minimax optimal control theory
Document ID
19680056598
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Johnson, C. D.
Redus, J. R.
Date Acquired
August 4, 2013
Publication Date
August 1, 1968
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Navigation
Report/Patent Number
AIAA PAPER 68-871
Report Number: AIAA PAPER 68-871
Meeting Information
Meeting: GUIDANCE, CONTROL, AND FLIGHT DYNAMICS CONFERENCE
Location: PASADENA, CA
Start Date: August 12, 1968
End Date: August 14, 1968
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
68A37570
Distribution Limits
Public
Copyright
Other

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