Wei Bosong, Li Cong, Dang Zhaohui, Yue Xiaokui
School of Astronautics, Northwestern Polytechnical University, 127 Youyi West Road, Xi'an 710072, China.
National Key Laboratory of Aerospace Flight Dynamics, Northwestern Polytechnical University, Xi'an 710072, China.
Sensors (Basel). 2025 Sep 8;25(17):5606. doi: 10.3390/s25175606.
The issue of in-orbit optimal safe surrounding control for service satellite (SSat) formation against a huge unknown target satellite (TSat) with specific structures is solved by using relative measurements only, and an optimal cooperative safe surrounding (OCSS) hybrid controller achieving both target tracking (TT) and configuration tracking (CT) is proposed corresponding to the two equal sub-objectives. Facing the challenges caused by incomplete information of the TSat, by using relative measurements only, the initial-condition-free boundaries are constructed by an arctan-based state transformation to directly constrain the target tracking error to perform prescribed transient and steady-state behaviors. Based on the shared TT control law, optimal collision-free CT controllers for all SSats are further solved via a nonzero-sum differential game, where the collision threat from all SSats and target structures are modeled by a novel circumscribed-sphere model. Finally, the effectiveness and advantages of the proposed OCSS control technique is verified by simulation results.
仅利用相对测量解决了服务卫星(SSat)编队针对具有特定结构的巨大未知目标卫星(TSat)的在轨最优安全环绕控制问题,并针对两个同等子目标提出了一种同时实现目标跟踪(TT)和构型跟踪(CT)的最优协同安全环绕(OCSS)混合控制器。面对由目标卫星信息不完整所带来的挑战,仅利用相对测量,通过基于反正切的状态变换构建无初始条件边界,以直接约束目标跟踪误差,使其执行规定的瞬态和稳态行为。基于共享的TT控制律,通过非零和微分博弈进一步求解所有服务卫星的最优无碰撞CT控制器,其中所有服务卫星与目标结构的碰撞威胁通过一种新颖的外接球模型进行建模。最后,通过仿真结果验证了所提OCSS控制技术的有效性和优势。