基于GPS/惯性导航的机载平台导引系统  

The Guidance System of Helicopter-Loaded Platform Based on GPS/Inertial Navigation

作　　者：廖鸣 

机构地区：[1]中国兵器工业第203研究所,西安710065

出　　处：《弹箭与制导学报》2005年第4期24-26,29,共4页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：在对机载设备进行靶场实验时,设备的承载平台往往需要对准目标,才能开始实验。为此,基于直升机的GPS和惯性导航系统,建立导引系统。该系统能实时解算出目标相对于机载平台的角偏差值,再通过伺服控制系统控制机载平台自动锁定目标。When the helicopter-loaded equipment is tested in the range, the test always can not be started until the equipment aim at the destination. On the base of helicopter＇s GPS ＆ Inertial Navigation System, We establish a guidance system, which real-time calculate the value of deviation angle between the target and helicopter-loaded platform. According to the angle, the helicopter-loaded platform will trace automatically under the control of servo system.

关 键 词：GPS/惯性 机载平台 导引系统 

分 类 号：V249.322[航空宇航科学与技术—飞行器设计]