摘要
本文结合弹道式地地导弹和运载器稳定平台提供的测量角度,研究了姿控系统的姿态角、框架角和旋转角之间,尤其是各偏差之间的关系,为正确实现姿态信号反馈,特别是大姿态控制提供了依据。
In this paper the research of the relations among attitude angles, frame angles and rotation angles, particularly between their deviations, is presented. Frame angles are measured from inertial stabilizing platforms mounted on in ground-to-ground ballistic missile and launch vehicle. Therefore the theoretical basis is established to implement correctlg attitude deviation feedbacks and particularly the large attitude control.
出处
《航天控制》
CSCD
北大核心
1992年第1期1-10,共10页
Aerospace Control
关键词
面对面导弹
运载火箭
姿态控制系统
Subject terms
Ground to ground missile
Launch vehicle
Attitude control system
