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Passivity-based adaptive attitude control of a rigid spacecraft

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2 Author(s)
Egeland, O. ; Div. of Eng. Cybern., Norwegian Inst. of Technol., Trondheim, Norway ; Godhavn, J.-M.

An adaptive control scheme for the attitude control of a rigid spacecraft is derived using a linear parameterization of the equation of motion. The tracking error is described with the Euler parameter vector. Global convergence of the tracking error to zero is shown using passivity theory. This allows for the use of time-varying positive-definite feedback gain matrices, and the results can easily be extended to other passive parameter update laws

Published in:

Automatic Control, IEEE Transactions on  (Volume:39 ,  Issue: 4 )

Date of Publication:

Apr 1994

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