文件名称:04699422SimulationSINS
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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 increments > aircraft during flight fly height unchanged > heading counterclockwise positive > in the Geography Department of the navigation fr a me > Run than the force required to import information and recommendations gyro angular rate information program
> 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 increments > aircraft during flight fly height unchanged > heading counterclockwise positive > in the Geography Department of the navigation fr a me > Run than the force required to import information and recommendations gyro angular rate information program
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04699422SimulationSINS
......................\SINS.m