Variable structure attitude maneuver and vibration control of flexible spacecraftOA
Variable structure attitude maneuver and vibration control of flexible spacecraft
A dual-stage control system design method is presented for the three-axis-rotational maneuver and vibration stabilization of a spacecraft with flexible appendages embedded with piezoceramics as sensor and actuator.In this des…查看全部>>
A dual-stage control system design method is presented for the three-axis-rotational maneuver and vibration stabilization of a spacecraft with flexible appendages embedded with piezoceramics as sensor and actuator.In this design approach,the attitude control and the vibration suppression sub-systems ale designed separately using the lower order model.The design of attitude controller is based on the variable structure control (VSC)theory leading to a discont…查看全部>>
HU Qing-lei;MA Cuang-fu
Dept.of Control Science and Engineering,Harbin Institute of Technology,Harbin 150001,ChinaDept.of Control Science and Engineering,Harbin Institute of Technology,Harbin 150001,China
航空航天
variable structure controlflexible spacecraftvibration controlattitude maneuver
variable structure controlflexible spacecraftvibration controlattitude maneuver
《哈尔滨工业大学学报（英文版）》 2008 (5)
一类挠性航天器主动振动鲁棒控制技术研究
705-710,6
Sponsored by the National Natural Science Foundation of China(Grant No.60774062),Research Fund for the Doctoral Program of Higher Education of China(Grant No.20070213061)and Young Excellent Talents in Harbin Institute of Technology(Grant No.HITQNJS.2007.001).
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