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.
出处
《弹箭与制导学报》
CSCD
北大核心
2005年第4期24-26,29,共4页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
GPS/惯性
机载平台
导引系统
OPS/Inertial
helicopter-loaded platform
guidance system
