Model predictive control for spacecraft rendezvous and docking with a rotating/tumbling platform and for debris avoidance
Model predictive control for spacecraft rendezvous and docking with a rotating/tumbling platform and for debris avoidance
复制标题
航天器与旋转/翻滚平台交会对接以及避免碎片的模型预测控制
DOI：
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发表时间：
2011
期刊：
影响因子：
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通讯作者：
I. Kolmanovsky
中科院分区：
文献类型：
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作者：
Hyeongjun Park;S. D. Cairano;I. Kolmanovsky
为航天器与旋转/翻滚平台的交会对接和碎片规避机动研究了一种模型预测控制方法。利用该方法，系统地研究了对接口视线锥内的推力、接近速度和航天器定位约束。的轨迹进行了模拟和时间停靠和燃料消耗的成本函数参数的变化进行评估。考虑了避免碎片的机动，碎片在航天器会合路径上。
A Model Predictive Control (MPC) approach is developed for spacecraft rendezvous and docking to a rotating/tumbling platform and for debris avoidance maneuvers. With this approach, the constraints on thrust, approach velocity and spacecraft positioning within the Line-of-Sight cone from the docking port are systematically treated. The trajectories are simulated and time-to-dock and fuel consumption are evaluated as cost function parameters are varied. Debris avoidance maneuvers are considered, with the debris in the spacecraft rendezvous path.