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Simulation and Design of Strapdown Inertial Navigation System Based on RT-Lab/Simulink

机译:基于RT-Lab / Simulink的捷联惯导系统仿真设计

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According to engineering characteristics which are huge construction quantities, long design period and high real time requirement of strapdown inertial navigation system (SINS), this paper introduces simulation of SINS based on Simulink and structure design of SINS based on RT-Lab. And implemented real-time simulation for RT-Lab after double sample of rotation vector on quaternion is used to attitude updating algorithm and double sample of compensated sculling error is used to velocity updating algorithm. Simulation results show that simulation method which based on RT-Lab/Simulink easy to realize of SINS, and overcome bad real time capability when simulation only use Matlab and large amounts of computation,long period and big error when simulation use C code which based on hardware.
机译:根据捷联惯性导航系统(SINS)的工程量大,设计周期长,实时性要求高的工程特点,介绍了基于Simulink的捷联惯导系统的仿真和基于RT-Lab的捷联惯导系统的结构设计。将四元数上的旋转矢量的两次采样用于姿态更新算法,并将补偿的划桨误差的两次采样用于速度更新算法,并对RT-Lab进行实时仿真。仿真结果表明,基于RT-Lab / Simulink的仿真方法易于实现捷联惯导系统,克服了仅使用Matlab进行仿真时实时性差,计算量大,使用基于C语言的C代码仿真时周期长,误差大的问题。硬件。

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