A Comparison of Nonlinear PI and PID Inertia-Free Spacecraft Attitude Control Laws
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Publisher
Springer Berlin Heidelberg
Link
http://link.springer.com/content/pdf/10.1007/978-3-662-44785-7_27
Reference23 articles.
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3. Ahmed, J., Coppola, V.T., Bernstein, D.S.: Asymptotic Tracking of Spacecraft Attitude Motion with Inertia Identification. AIAA J. Guid. Contr. Dyn. 21, 684–691 (1998)
4. Wen, J.T.Y., Kreutz-Delgado, K.: The Attitude Control Problem. IEEE Transactions on Automatic Control 36, 1148–1162 (1991)
5. Bhat, S.P., Bernstein, D.S.: A Topological Obstruction to Continuous Global Stabilization of Rotational Motion and the Unwinding Phenomenon. Sys. Contr. Lett. 39, 63–70 (2000)
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