NSSC OpenIR  > 空间技术部
Alternative TitleCoordinated Attitude Control and Simulation of Formation Flying Satellites
李宏枫; 郑建华; 高东; 北京8701信箱
Source Publication计算机仿真
Keyword编队飞行 姿态协同控制 姿态四元素
Other AbstractFor solving the coordinated attitude control problem of three satellite formation flying imaging radar altimeter is designed used for earth-observation, the attitude control system is designed and the simulation research is made based on attitude quaternion. Firstly,the reference coordinates and attitude error variables are defined.Secondly, a kind of non-linear attitude tracking controller is designed, and the global stability of the control law is p roved by using Lyapunov stability theory.Lastly,through simulation based on Matlab and visualization based on STK, the stability and validity of the control law are validated.The simulation result indicates that the method enables the following satellite in the formation to track the leading satellite at any time. It is also to say that the method can realize the goal of the synthetic aperture interferometry task.
Indexed ByCSCD
Funding Project中国科学院空间科学与应用研究中心
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Document Type期刊论文
Corresponding Author北京8701信箱
Recommended Citation
GB/T 7714
李宏枫,郑建华,高东,等. 小卫星编队飞行姿态协同控制及仿真[J]. 计算机仿真,2008,25(8):44-46,50.
APA 李宏枫,郑建华,高东,&北京8701信箱.(2008).小卫星编队飞行姿态协同控制及仿真.计算机仿真,25(8),44-46,50.
MLA 李宏枫,et al."小卫星编队飞行姿态协同控制及仿真".计算机仿真 25.8(2008):44-46,50.
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