An optimal slewing maneuver approach for a class of spacecraft with flexible appendages
Author:
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference8 articles.
1. Poles and transmission zeros of flexible spacecraft control systems;Kida;J. Guidance Control Dynam.,1985
2. Optimal distributed control of a flexible spacecraft during a large-angle maneuver;Turner;J. Guidance Control,1984
3. Optimal feedback slewing of flexible spacecraft;Breakwell;J. Guidance Control,1981
4. Closed-form solutions for feedback control with terminal constraints;Juang;J. Guidance Control Dynam.,1985
5. Applied Optimal Control.;Bryson,1975
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2. Characteristic Model-based Fast Attitude Maneuver for the Complex Flexible Satellite;AIAA SPACE 2015 Conference and Exposition;2015-08-28
3. Vibration suppression and adaptive-robust control of a smart flexible satellite with three axes maneuvering;Acta Astronautica;2011-09
4. Optimization of generalized potential in mission function control - Analytical and experimental results;Journal of Guidance, Control, and Dynamics;1996-01
5. An active vibration suppression method for the flexible spacecrafts and its application;Astrodynamics Conference;1994-08-01
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