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su lv jie lian kong zhi xi tong chu shi zhi jie suan
Author(s): 
Pages: 51-54
Year: Issue:  1
Journal: Aerospace Control

Keyword:  捷联速率积分陀螺仪控制系统加速度表微型计算机法向加速度采样周期惯导伺服机构阵风干扰;
Abstract: <正> 速率捷联控制系统主要是由与弹体捷联的速率积分陀螺仪,摆式加速度表以及微型计算机,伺服机构组成。这类系统在飞行中要完成稳定与制导的任务,首先需要求解弹体坐标系的初始值。对于地一地导弹或运载火箭来说,就是必须首先解算出发射瞬时,弹体坐标系
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