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Design of simulation and verification system for rotation strapdown inertial navigation system

机译:旋转捷联惯性导航系统仿真验证系统设计

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Aiming at the problem that quantitative error analysis of strapdown inertial navigation system (SINS) caused by key error cannot be achieved, this paper accomplished the design of simulation and verification system for the single-axis continuous and the to-and-fro rotation SINS. By simulating inertial measurement unit (IMU) outputting information in different single-axis rotation methods, the principle error of SINS is simulated and validated. By designing algorithm to compensate IMU errors online, the actual rotation SINS error caused by IMU random drift error, scale factor error and installation error can be optimized. In this paper, design of individual algorithmic process and functional module are illustrated. The test results show the simulation and verification system can carry out the simulation for the rotation SINS scheme well, and can provide effective support for improvement of rotation scheme technically.
机译:针对无法实现由关键误差引起的捷联惯性导航系统(SINS)定量误差分析的问题,本文完成了单轴连续和往复旋转捷联惯导系统的仿真验证系统的设计。通过模拟惯性测量单元(IMU)以不同的单轴旋转方式输出信息,对捷联惯导系统的原理误差进行了仿真和验证。通过设计在线补偿IMU误差的算法,可以优化由IMU随机漂移误差,比例因子误差和安装误差引起的实际旋转SINS误差。本文阐述了单个算法过程和功能模块的设计。测试结果表明,该仿真验证系统可以很好地对旋转惯导系统进行仿真,从技术上可以为旋转方案的改进提供有效的支持。

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