Control of Attitude and Vibration of a Tethered Space Solar Power Satellite
Author:
Affiliation:
1. Tokyo Metropolitan Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-5421
Reference39 articles.
1. and Experimental Investigation of Space-Realizable Inertial Actuation for Passive and Active Structural Control," Journal of Guidance, Control, and Dynamics, Vol.11, No.5,Sept.Oct. 1988, pp.449-458.
2. Suboptimal feedback vibration control of a beam with a proof-mass actuator
3. Nonlinear Control of a Proof-Mass Actuator
4. Passive Control of Multi-Degree of Freedom Systems Using a Vibration Absorber," AIAA-90-3499-CP, 1990.
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