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Improved reference trajectory generation method in reentry guidance

机译:再入制导中改进的参考轨迹生成方法

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摘要

After generating reference trajectory in the process of reentry guidance for reusable launch vehicle, if the designed bank angle curve is too close to the constraint boundary, there is a great possibility for the obtained reference trajectory to exceed the reentry corridor boundary. This paper proposed a margin searching method, to reduce the likelihood of generating a reference trajectory which exceeds the reentry corridor boundary and to improve the design success rate.
机译:在可重复使用运载火箭的再入引导过程中生成参考轨迹后,如果设计的倾斜角曲线太靠近约束边界,则获得的参考轨迹很有可能会超过再进入通道边界。本文提出了一种边距搜索方法,以减少产生超过折返通道边界的参考轨迹的可能性,并提高设计成功率。

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