The integrated system is composed of SINS and GPS, each subsystem's navigational parameter is sent to navigation computer. At there the azimuth and attitude angle error is estimated by Kalman filter, then be used to adjust the attitude matrix of SINS. 组合系统由SINS、GPS两个系统构成,各子系统的导航信息输出至导航计算机,应用卡尔曼滤波方法估计三个方向的失准角,并对SINS系统的姿态矩阵进行校正。
The main task is the PC design of airport navigational lights computer monitoring system, the paper has also carried a certain amount of research about under-machine design of airport navigational lights computer monitoring system. 主要任务是机场助航灯计算机监控系统上位机的设计,本论文对机场助航灯计算机监控系统下位机的设计也进行了一定的研究。
Navigational lights computer monitoring system plays an essential role in the safety of aircraft taking off and landing, it is the navigation facilities to protect aircraft in low visibility at night and other complex weather conditions to take off, land and taxiing smoothly. 助航灯光计算机监控系统对飞机的安全起降起着至关重要的作用,它是保障飞机在夜间能见度非常低和复杂天气情况下能顺利起飞、着陆以及滑行的导航设施。