本文主要研究内容
作者（2019）在《New Iterative Guidance for Launch Vehicle with Quadratic Optimization》一文中研究指出：This paper investigates the iterative guidance mode for launch vehicle. In order to improve the precision of the guidance system and minimize the flight time, the iterative guidance mode derived from
Abstract
This paper investigates the iterative guidance mode for launch vehicle. In order to improve the precision of the guidance system and minimize the flight time, the iterative guidance mode derived from
论文参考文献
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论文详细介绍
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标签：第31届中国控制与决策会议2019-06-03论文;
：New Iterative Guidance for Launch Vehicle with Quadratic Optimization论文
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