The invention relates to an agile satellite quantifiable control same-orbit multi-strip splicing planning method. The method comprises the following steps: constructing a search solution space; calling a parallel tracking diffusion search mode by utilizing a genetic algorithm solution space search framework to search a feasible solution of the agile satellite same-orbit multi-strip splicing planning scheme in the search solution space; performing quality evaluation on the feasible solution based on quantitative analysis of a strip overlapping rate; and the optimal scheme of the agile satellite common-orbit multi-strip splicing planning is obtained by iterating the searching and evaluation process of the feasible solution for multiple times. According to the method, on the basis of meeting the satellite common-orbit multi-time observation attitude maneuver constraint, quantitative analysis and quantitative control of the strip overlapping rate are achieved, and a relative optimal strip splicing scheme meeting expectation is obtained through rapid searching in a solution space.
本发明涉及一种敏捷型卫星可量化控制同轨多条带拼接规划方法,包括:构造搜索解空间;利用遗传算法解空间搜索框架调用并行跟踪扩散搜索模式在所述搜索解空间内搜索敏捷型卫星同轨多条带拼接规划方案的可行解;基于条带重叠率的量化分析,对所述可行解进行优劣评价;通过多次迭代可行解的搜索和评价过程,得到敏捷型卫星同轨多条带拼接规划的最优方案。本发明在满足卫星同轨多次观测姿态机动约束的基础上,实现条带重叠率的定量分析和量化控制,在解空间中快速搜索得到满足预期的相对最优条带拼接方案。
Agile satellite quantifiable control co-orbit multi-strip splicing planning method
敏捷型卫星可量化控制同轨多条带拼接规划方法
2023-06-27
Patent
Electronic Resource
Chinese
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