球载姿态测量系统研究  

Research on Ball-borne Attitude Measuring System

作　　者：罗山[1,2] 李勇建[3] 李星海[3] 冯伟[3] 

机构地区：[1]空军工程大学导弹学院,陕西西安710051 [2]空军驻重庆气体压缩机厂军事代表室,重庆400060 [3]四川压电与声光技术研究所,重庆400060

出　　处：《压电与声光》2009年第1期31-33,共3页Piezoelectrics & Acoustooptics

摘　　要：升空气球作为空间飞行器,其价格比飞机低,在空中停留时间比飞机长,利用升空气球装载雷达等电子设备在高空中可长期工作,因此,升空气球在军事和民用上的应用前景广,而作为升空气球球载设备姿态测量的惯性系统研究是很有必要的。我们针对球载设备姿态测量进行了研究,设计了适用的捷联惯性/GPS组合导航系统,可提供升空气球球载设备姿态测量和控制需要的气球航向、俯仰及滚动等姿态参数,满足了球载设备长期工作要求和升空气球应用特点。As a spacecraft, the price of the blastoff-balloon is much lower than plane and it stays much longer in the space. The blastoff-balloon equipped with radar or other electronic equipment can work for longer time in the air, so it will be used widely in military and civilian field. It is necessary to research it, which takes with SINS to measure attitude. For this, we have carried out special study, and have designed a useful SINS/GPS integrated navi- gation system, it can provide yaw,pitch and roll angle for measuring and controlling attitude. It meets the request of long-term work and conforms for the application characteristic of blastoff-balloon. It has been used successfully.

关 键 词：升空气球 捷联惯性 GPS 组合导航 姿态测量系统 

分 类 号：V249[航空宇航科学与技术—飞行器设计]