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Globally stable control laws for the attitude maneuver problem - Tracking control and adaptive controlAn approach using a globally nonsingular representation is proposed for the attitude control problem of a rigid body. The attitude dynamics are described by the nonlinear Euler equation together with the nonlinear kinematic equations which relate a representation of attitude to the angular velocity of the body. When this approach is combined with an energy-motivated Lyapunov function, a large class of globally stable attitude control laws can be derived. This class includes model-independent tracking control, model-dependent tracking control, and adaptive control, allowing tradeoffs between controller complexity, attainable performance, and available model information.
Document ID
19890041127
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wen, John T.
(Rensselaer Polytechnic Institute, Troy, NY, United States)
Kreutz, Kenneth
(California Institute of Technology Jet Propulsion Laboratory, Pasadena, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1988
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: IEEE Conference on Decision and Control
Location: Austin, TX
Country: United States
Start Date: December 7, 1988
End Date: December 9, 1988
Accession Number
89A28498
Distribution Limits
Public
Copyright
Other

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