Because the real input acceleration can not be obtained during the error model identification of the inertial navigation platform, so the measurement value is used to substitute the input data.
在进行惯导平台误差模型辨识的过程中，真实的输入加速度难以获得，因此不得不使用测量值来代替，这使得输入输出观测数据中均含有测量噪声。
The design of gyroscope data acquisition system for Marine strapdown inertial navigation system is presented.
介绍了船用捷联惯性导航系统中陀螺仪数据采集系统的设计。
The experiment data of GPS/INS integrated navigation system as well as main error source of inertial parts has been analyzed.
利用了一种管道地理位置测量的有效方法，即GPS/INS组合导航系统，对组合导航系统的实验数据进行了分析。
In order to realize high speed data communication between missile-borne computer and inertial navigation system, the engineering circuitry of data communication is designed.
为了实现弹载计算机和惯导的高速数据通信，对数据通信的工程化电路进行了设计。
In order to realize high speed data communication between missile-borne computer and inertial navigation system, the engineering circuitry of data communication is designed.
为了实现弹载计算机和惯导的高速数据通信，对数据通信的工程化电路进行了设计。
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