Square root state estimator for large space structures
Author:
Affiliation:
1. New York, State University, Buffalo
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1987-2389
Reference24 articles.
1. Likins, P.W., The Application of Multivariable ControlTheory to Spacecraft Attitude,' Proc. IFAC4th Internationel SymposiumonMu 1ti-variableTechnological Systems, NewBrunswick, Canada, June 1977, pp.11-20.
2. Jusng. Jer-Nan, L.G. HortaandH.H. Robertshaw, 'A SlewingControl Experiment for Flexible Structures,' J.Guidance, Control and Dynamics, Vol.9, No.5, Sept.Oct. 86, pp.599-607.
3. Hughes, P.C. andR.E. Skelton, 'Controllability and Observability of Linear Matrix-Second-Order Systems,' J.Applied Mechanics, Vol.47, June 80, pp.415-420. 1 6 Hughes, P.C. andR.E. Skelton, 'Controllability and Observability for FlexibleSpacecraft,'J. Guidance andControl, Vol. 3, No. 5, Sept.Oct. 80, pp. 452-459.
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