REDUNDANT ATTITUDE CONTROL SYSTEM FOR THE UNPOWERED 3~(rd) STAGE OF THE SHAVIT LAUNCHER

机译：剃须刀发射器未启动的3〜（rd）阶段的冗余姿态控制系统

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This article presents the design of a redundant, three-axis attitude control system (ACS) of the Shavit space launcher. The ACS consists of two independent systems, each one capable controlling the pitch/yaw axes, while only one controls the roll axis. Selection/intervention logic between the systems must be chosen. Two types of intervention logic are discussed: passive intervention and fault-detection. It is shown, that passive intervention in pitch/yaw coupled with active identification in roll is the better choice. The selected logic is demonstrated through simulations and in-flight performance.

机译：本文介绍了Shavit空间发射器的冗余三轴姿态控制系统（ACS）的设计。 ACS由两个独立的系统组成，每个系统都可以控制俯仰/偏航轴，而只有一个系统可以控制侧倾轴。必须选择系统之间的选择/干预逻辑。讨论了两种干预逻辑：被动干预和故障检测。结果表明，俯仰/偏航的被动干预与侧倾的主动识别相结合是更好的选择。所选逻辑通过仿真和飞行中的性能进行演示。

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《48th Israel Annual Conference on Aerospace Sciences 2008》|2008年|P.704720|共2页
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Klots M.; Goldstein M.; Kahane A.; Levy Y.;
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中图分类航空;
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REDUNDANT ATTITUDE CONTROL SYSTEM FOR THE UNPOWERED 3~(rd) STAGE OF THE SHAVIT LAUNCHER

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