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Laws For Stable Control Of OrientationClass of globally stable laws for control of orientation of rigid body established. Tradeoffs made among complexity, performance, and information available for mathematical models. New approach involves use of globally nonsingular four-parameter unit-quaternion (Euler-parameter) representation. Attitude dynamics described by nonlinear Euler equation together with nonlinear kinematic equations, which relate representation of attitude to angular velocity of body. Suitable energy-motivated Lyapunov function to analyze stability.
Document ID
19900000430
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Kreutz, Kenneth K.
(Caltech)
Wen, John Ting-Yung
(Rensselaer Polytechnic Inst.)
Date Acquired
August 14, 2013
Publication Date
August 1, 1990
Publication Information
Publication: NASA Tech Briefs
Volume: 14
Issue: 8
ISSN: 0145-319X
Subject Category
Mathematics And Information Sciences
Report/Patent Number
NPO-17790
Accession Number
90B10430
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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