Preshaping Profiler for Flexible Spacecraft Rest-to-Rest Maneuvers
Author:
Affiliation:
1. NEC Toshiba Space Systems, Ltd.
2. Japan Aerospace Exploration Agency
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-6181
Reference7 articles.
1. Time-Optimal Negative Input Shapers
2. Preshaping Command Inputs to Reduce System Vibration
3. Extra-insensitive input shapers for controlling flexible spacecraft
4. Robust time-optimal control of uncertain flexible spacecraft
5. Planar, time-optimal, rest-to-rest slewing maneuvers of flexible spacecraft
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1. Discrete-Time Nonlinear Attitude Tracking Control of Spacecraft;Gyroscopes - Principles and Applications;2020-05-20
2. Nonlinear model predictive control applied to spacecraft attitude control (Closed-loop stability and optimality with thrusters and wheels);Transactions of the JSME (in Japanese);2016
3. Agile and Precise Attitude Switching Maneuver of Flexible Spacecraft based on Nonstationary Frequency-Shaped Robust Control;Journal of System Design and Dynamics;2011
4. Design of Reference for High-Speed and Vibration-Less Attitude Maneuvering of Flexible Satellite;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2010
5. A Preliminary Study on Precise Attitude Switching Maneuver of Flexible Spacecraft Using CMG;Journal of Space Engineering;2009
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