首页> 美国政府科技报告 >Design and Fabricate Rocket Attitude Control System (ACS) for Accurate Payload Orientation and Control Functions.
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Design and Fabricate Rocket Attitude Control System (ACS) for Accurate Payload Orientation and Control Functions.

机译:设计和制造火箭姿态控制系统(aCs),实现精确的有效载荷定位和控制功能。

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摘要

Three (3) Attitude Control Systems (ACS) were designed and built for SPICE, IRBS, ZIP, and FIRSSE (Background Measurements) programs. They utilized star tracker, IRU, and MIDAS platforms. The IRU system gives state-of-the-art accuracy. (Author)

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