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首页> 外文期刊>Advances in space research >Collision avoidance ZEM/ZEV optimal feedback guidance for powered descent phase of landing on Mars
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Collision avoidance ZEM/ZEV optimal feedback guidance for powered descent phase of landing on Mars

机译:避免碰撞ZEM / ZEV针对火星着陆动力下降阶段的最佳反馈指导

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摘要

A novel zero-effort-miss (ZEM)/zero-effort-velocity (ZEV) optimal feedback guidance is proposed in order to rule out the possibility of Martian surface collision caused by the classical ZEM/ZEV optimal feedback guidance. The main approach is to add a collision avoidance term, which has self-adjustment capacity to ensure the near fuel optimality. Its main improvement is that it can not only successfully avoid collisions with the thruster constraint but also guarantee the near fuel optimality, and both of them are pivotal performances in Mars landing missions. Simulations are made to show the effectiveness of the proposed guidance and the parameters effects are simulated as well to analyze the properties of the proposed guidance.
机译:为了排除经典的ZEM / ZEV最优反馈导引引起的火星表面碰撞的可能性,提出了一种新型的零努力缺失(ZEM)/零努力速度(ZEV)最优反馈指导。主要方法是增加一个避免碰撞项,该项具有自我调节能力以确保接近燃料的最优性。它的主要改进是,它不仅可以成功避免与推进器约束发生碰撞,而且还可以保证接近燃油的最优性,这两者都是火星着陆任务中的关键性能。仿真表明了该指导的有效性,并对参数效果进行了仿真,以分析该指导的特性。

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