Variable-structure control of spacecraft attitude maneuvers
- 1 May 1988
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 11 (3) , 262-270
- https://doi.org/10.2514/3.20303
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Exact nonlinear control of spacecraft slewing maneuvers with internal momentum transferJournal of Guidance, Control, and Dynamics, 1986
- Variable-structure control of spacecraft large-angle maneuversJournal of Guidance, Control, and Dynamics, 1986
- Quaternion feedback for spacecraft large angle maneuversJournal of Guidance, Control, and Dynamics, 1985
- Exact nonlinear control of large angle rotational maneuversIEEE Transactions on Automatic Control, 1984
- Global transformations of nonlinear systemsIEEE Transactions on Automatic Control, 1983
- Spacecraft large angle rotational maneuvers with optimal momentum transferPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Optimal feedback slewing of flexible spacecraftJournal of Guidance and Control, 1981
- Optimal Continuous Torque Attitude ManeuversJournal of Guidance and Control, 1980
- Controller Design for a Manipulator Using Theory of Variable Structure SystemsIEEE Transactions on Systems, Man, and Cybernetics, 1978