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Vibration reduction for flexible spacecraft following momentum dumping with/without slewing

机译：在有/无回转的动量倾卸之后，柔性航天器的减振

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Arun K. Banerjee; Nelson Pedreiro; William E. Singhose;
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年度 2001
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1. Continuous robust fault-tolerant control and vibration suppression for flexible spacecraft without angular velocity [J] . Zhang Xiuyun, Zong Qun, Tian Bailing, International Journal of Robust and Nonlinear Control . 2019,第12期

机译：对于无角速度的柔性航天器，持续稳健的容错控制和振动抑制
2. Robust Adaptive Attitude Tracking Control With L2-Gain Performance and Vibration Reduction of an Orbiting Flexible Spacecraft [J] . Qinglei Hu Journal of Dynamic Systems, Measurement, and Control . 2011,第1期

机译：具有L2增益性能和减震特性的鲁棒自适应姿态跟踪控制
3. Simultaneous vibration reduction and attitude control of flexible spacecraft with on-off actuators [J] . QInglei Hu Intelligent automation and soft computing . 2011,第3期

机译：带有开关执行器的挠性航天器同时减振和姿态控制
4. Vibration Reduction for Flexible spacecraft following momentum dumping with/without slewing [C] . Arun K.Banerjee, Nelson Pedreiro, William Singhose AAS/AIAA astrodynamics conference . 2000

机译：振动减少柔性航天器跟随/无回转
5. Modeling and slew-maneuver control of a flexible spacecraft. [D] . Eckhart, Jeremy E. 2005

机译：挠性航天器的建模和回转操纵控制。
6. Experimental Study on the Effectiveness of Polyurethane Flexible Adhesive in Reduction of Structural Vibrations [O] . Natalia Lasowicz, Arkadiusz Kwiecień, Robert Jankowski 2020

机译：基于结构振动减少聚氨酯柔性粘合剂的实验研究
7. Vibration Reduction for Flexible Spacecraft Attitude Control Using PWPF Modulator and Smart Structures [O] . Song G., Agrawal B.N. 1999

机译：使用PWPF调制器和智能结构的柔性航天器姿态控制减震
8. VIBRATION OF A FLEXIBLE SPACECRAFT WITH MOMENTUM EXCHANGE CONTROLLERS [R] . Joseph Reed Canavin 1976

机译：用动量交换控制器对柔性航天器进行振动

Vibration reduction for flexible spacecraft following momentum dumping with/without slewing

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