Active vibration control synthesis for the control of flexible structures mast flight system
- 1 May 1988
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 11 (3) , 271-277
- https://doi.org/10.2514/3.20304
Abstract
No abstract availableKeywords
This publication has 9 references indexed in Scilit:
- A new concept of generalized structural filtering for active vibration control synthesisPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Multivariable control robustness examples - A classical approachJournal of Guidance, Control, and Dynamics, 1987
- Microprocessor controlled force actuatorPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Roll/yaw control of a flexible spacecraft using skewed bias momentumwheelsJournal of Guidance, Control, and Dynamics, 1985
- Experiments in control of flexible structures with noncolocated sensors and actuatorsJournal of Guidance, Control, and Dynamics, 1984
- Attitude stabilization of flexible spacecraft during stationkeeping maneuversJournal of Guidance, Control, and Dynamics, 1984
- Design of the Galileo scan platform controlJournal of Guidance, Control, and Dynamics, 1984
- Some Connections Between Modern and Classical Control ConceptsJournal of Dynamic Systems, Measurement, and Control, 1979
- Control System Design in the Presence of Severe Structural Dynamics InteractionsJournal of Guidance and Control, 1978