Optimal simultaneous structural and control design of maneuvering flexible spacecraft
- 1 January 1985
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 8 (1), 86-93
- https://doi.org/10.2514/3.19939
Abstract
No abstract availableKeywords
This publication has 11 references indexed in Scilit:
- Robust control of self-adjoint distributed-parameter structuresJournal of Guidance, Control, and Dynamics, 1984
- Control of Self -Adj oint Distributed-Parameter SystemsJournal of Guidance, Control, and Dynamics, 1982
- Optimal feedback slewing of flexible spacecraftJournal of Guidance and Control, 1981
- Optimal Control of Damped Flexible Gyroscopic SystemsJournal of Guidance and Control, 1981
- Optimal Local Control of Flexible StructuresJournal of Guidance and Control, 1981
- Optimization with Vector — Valued CostPublished by Springer Science and Business Media LLC ,1981
- Optimal Large-Angle Single-Axis Rotational Maneuvers of Flexible SpacecraftJournal of Guidance and Control, 1980
- Modal-Space Control of Distributed Gyroscopic SystemsJournal of Guidance and Control, 1980
- Feedback control of flexible systemsIEEE Transactions on Automatic Control, 1978
- Active control of flexible systemsJournal of Optimization Theory and Applications, 1978