Maneuver and vibration control of SCOLE
- 1 November 1988
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 11 (6) , 542-553
- https://doi.org/10.2514/3.20351
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- Limited evaluation of the longitudinal flying qualities of a centerstick aircraft with variations in stick feel parametersJournal of Guidance, Control, and Dynamics, 1987
- Equations of motion for maneuvering flexible spacecraftJournal of Guidance, Control, and Dynamics, 1987
- Nonlinear natural control of an experimental beamJournal of Guidance, Control, and Dynamics, 1984
- Optimal distributed control of a flexible spacecraft during a large-angle maneuverJournal of Guidance, Control, and Dynamics, 1984
- Globally optimal control of self‐adjoint distributed systemsOptimal Control Applications and Methods, 1983
- 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 Large-Angle Single-Axis Rotational Maneuvers of Flexible SpacecraftJournal of Guidance and Control, 1980