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与非合作目标编队的相对姿态控制 被引量:2

Relative Attitude Control in Non-cooperative Target Formation Flying
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摘要 针对非合作目标卫星编队飞行过程中,根据任务需要受控卫星保持指目标卫星。为了跟踪目标姿态,提出了一种相对姿态控制方法。该算法只需测量目标的相对位置,通过计算得到目标姿态。然后设计了相对角速度观测器,得到相对角速度,通过跟踪控制器实现无误差姿态跟踪。完整相对姿态控制任务包括姿态机动和姿态跟踪两部分,因此设计了混合控制器实现被控星的姿态机动和对目标姿态的动态跟踪。数值仿真结果表明该方法可以实现对运动目标的无差快速跟踪。 In non-cooperative target formation,the controlled satellite keeps pointing to the moving target on the basis of requirement of missions.To track a moving target,an approach is presented.It requires only relative positions and target attitude is computed with them.Then a relative angular velocity observer is designed and relative angular velocity is available.Attitude tracking without errors is accomplished by attitude tracking controller.Since a complete relative attitude control is composed of angle maneu...
出处 《宇航学报》 EI CAS CSCD 北大核心 2007年第5期1210-1214,共5页 Journal of Astronautics
基金 973国家安全重大基础研究(5131201) 863国防高技术支持(2002AA715021)
关键词 编队飞行 相对姿态 非合作目标 姿态跟踪 Satellite formation flying Relative attitude Non-cooperative target Attitude tracking
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参考文献5

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同被引文献21

  • 1宋斌,李传江,马广富.航天器姿态机动的鲁棒自适应控制器设计[J].宇航学报,2008,29(1):121-125. 被引量:15
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  • 3胡庆雷,马广富,姜野.控制受限的挠性航天器姿态机动自适应变结构输出反馈控制[J].宇航学报,2007,28(4):875-879. 被引量:8
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  • 6KRISTIANSEN R, NICKLASSON P, GRAVDAHL J. Spacecraft co- ordination control in 6DOF: integrator backstepping vs passivity- based control [J]. Automatica, 200,8, 44(11): 2896 - 2901.
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  • 8KIM K, KIM Y. Robust backstepping control for slew maneuver us- ing nonlinear tracking function [J]. IEEE Transactions on Control Systems Technology, 2003, 11 (6): 822 - 829.
  • 9ALl I, RADICE G, KIM J. Backstepping control design with actuator torque bound for spacecraft attitude maneuver [J]. Journal of Guid- ance Control and Dynamics, 2010, 33(1): 254- 259.
  • 10HU Qinglei. Robust adaptive backstepping attitude and vibration con- trol with L2-gain performance for flexible spacecraft under angular velocity [J]. Journal of Sound and Vibration, 2009, 327(3/5): 285 - 298.

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