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Exponential Time-varying Sliding Mode Control for Large Angle Attitude Eigenaxis Maneuver

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Exponential Time-varying Sliding Mode Control for Large Angle Attitude Eigenaxis Maneuver of Rigid

Spacecraft

Cong Binglong;Liu Xiangdong;Chen Zhen

【期刊名称】《中国航空学报:英文版》 【年(卷),期】2010(000)004

【摘要】^10F;中国航空学报:英文版 【总页数】7页(P.447-453)

【关键词】大角度姿态机动;滑模控制;航天器;刚性;时变;Lyapunov方法;参数不确定性;外部干扰

【作者】Cong Binglong;Liu Xiangdong;Chen Zhen 【

School;of;Automation,;Beijing;Institute;of;Technology,;Beijing;100081,;China

【正文语种】英文 【中图分类】TP273 【相关文献】

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LIU XiangDong; QIU Wei; HOU ChaoZhen

3.Adaptive Integral-type Sliding Mode Control for Spacecraft Attitude Maneuvering Under Actuator Stuck Failures [J], HU Qinglei; ZHANG Youmin; HUO Xing; XIAO Bing

4.Study of engaged performance regulation in controlled transfer clutch of 4WD car based on genetic sliding mode control [J], Zhang Yang; Men Yongxin; Li Wei; Ma Mingtu

5.Control of the DC Output Voltage of the AC/DC Converter Using Sliding Mode Control: Application to PMSG [J], H. Chennoufi; L. Louze; A.L. Nemmour; A. Khezzar

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Exponential Time-varying Sliding Mode Control for Large Angle Attitude Eigenaxis Maneuver

ExponentialTime-varyingSlidingModeControlforLargeAngleAttitudeEigenaxisManeuverofRigidSpacecraftCongBinglong;LiuXiangdong;ChenZhen【期刊名称】《中国航空学报:英文版》【
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