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航天飞机制导-导航控制 被引量:1

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摘要 本文根据航天飞机各个飞行阶段的具体条件概述了航天飞机制导-导航控制系统的控制要求。分析了各飞行阶段可能采用的制导-导航控制装置及其分系统,并说明冗余系统数据选取办法。同时,还论述了各种可用的制导-导航控制技术,比较了它们的优缺点。最后,概述了有关航天飞机制导-导航控制系统的可靠性设计问题。
作者 张谦
出处 《航天控制》 CSCD 北大核心 1989年第3期11-19,共9页 Aerospace Control
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