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Tracking functions applied to the determination of the asymptotic behavior of a space station

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1 Author(s)
J. Hewit ; University of Newcastle upon Tyne, Newcastle upon Tyne, England

Bounds on the response of the roll axis motion of an inertially oriented space station are obtained using the tracking function method. The use of a single complicated Lyapunov function is replaced by consideration of a number of very simple functions and the analysis is simplified and enhanced. Indication is given of how to apply the method to the motion about other axes.

Published in:

IEEE Transactions on Automatic Control  (Volume:20 ,  Issue: 5 )