Attitude stabilization of a rigid spacecraft using two control torques: A nonlinear control approach based on the spacecraft attitude dynamics

Attitude stabilization of a rigid spacecraft using two control torques: A nonlinear control approach based on the spacecraft attitude dynamics

10.1016/0005-1098(94)90196-1

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Bibliographic Details
Main Authors: Krishnan, H., Reyhanoglu, M., McClamroch, H.
Other Authors: MECHANICAL & PRODUCTION ENGINEERING
Format: Article
Published: 2014
Subjects:
Attitude control
Discontinuous feedback
Spacecraft stabilization
Online Access:http://scholarbank.nus.edu.sg/handle/10635/57940
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Institution: National University of Singapore
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