Input-shaped control of three-dimensional maneuvers of flexible spacecraft
- 1 November 1993
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 16 (6) , 1061-1068
- https://doi.org/10.2514/3.21128
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Robust Time-Delay ControlJournal of Dynamic Systems, Measurement, and Control, 1993
- Use of the work-energy rate principle for designing feedback controllawsJournal of Guidance, Control, and Dynamics, 1992
- Mission function control for a slew maneuver experimentJournal of Guidance, Control, and Dynamics, 1991
- Preshaping Command Inputs to Reduce System VibrationJournal of Dynamic Systems, Measurement, and Control, 1990
- Mechanics And Control Of Large Flexible StructuresPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Quarternion feedback regulator for spacecraft eigenaxis rotationsJournal of Guidance, Control, and Dynamics, 1989
- On undershoot and nonminimum phase zerosIEEE Transactions on Automatic Control, 1986