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Spacecraft optimal control theory, as well as optimal guidance law

space:nowrap;">航天器最优控制理论,是在满足一定约束条件下,寻求最优控制策略,使得性能指标取极大值或极小值。以航天器交会对接最优制导律设计与仿真为例,阐释最优控制的算法流程以及设计思想...


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