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Orbit attitude control device, and method of controlling orbit attitude

机译:轨道姿态控制装置及控制轨道姿态的方法

摘要

An orbit attitude control device includes a plurality of nozzles for injecting combustion gas supplied from a combustion chamber, and a control section configured to calculate nozzle opening degree correction values so that a deviation between a detection value of the pressure of the combustion chamber and a command value becomes smaller. The control section is configured to calculate a total correction value so that the deviation between the detection value and the command values becomes smaller. A total value T1 for first group nozzles and a total value T2 for second group nozzles are calculated. The total correction value is distributed to the opening degree correction values for the first group nozzles with a ratio of T2/(T1+T2) and to the opening degree correction values for the second group nozzles with a ratio of T1/(T1+T2).
机译:轨道姿态控制装置包括:多个喷嘴,其用于喷射从燃烧室供应的燃烧气体;以及控制部,其被构造为计算喷嘴开度校正值,使得燃烧室的压力的检测值与指令之间存在偏差。值变小。控制部分被配置为计算总校正值,使得检测值和命令值之间的偏差变小。计算第一组喷嘴的总值T 1 和第二组喷嘴的总值T 2 。总校正值以T 2 /(T 1 + T 2 的比率分配到第一组喷嘴的开度校正值>)和第二组喷嘴的开度校正值,其比率为T 1 /(T 1 + T 2 )。

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