A design technique for determining actuator gains in spacecraft vibration control
- 15 April 1985
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Optimum actuator placement, gain, and number for a two-dimensional grillagePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Optimum damping locations for structural vibration controlPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982