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04699422SimulationSINS
- 此为基于四元素法,角增量法的捷连惯导系统程序算法 > 飞行器飞行过程中飞行高度不变 > 航向角以逆时针为正 > 以地理系为导航坐标系 > 运行程序时需导入比力信息及陀螺议角速率信息-This is based on the Czech Republic and even the four elements Inertial Navigation System program algorithm method, a method of angular