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Error Analysis and Simulation of the Dual-axis Rotation-dwell Autocompensating Strapdown Inertial Navigation System

机译:双轴旋转停留自动补偿捷联惯导系统误差分析与仿真

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The error divergence of the strapdown inertial navigation system (INS) could be restrained through systemic rotation autocompensation technique. This technique could effectively bring system better precision performance without using higher precision gyros and accelerometers. An eightposition dual-axis rotation-dwell scheme is introduced, and system error equation is derived and analyzed. By implementing this scheme the behaviors of some errors change. Error analysis shows that the system error caused by constant bias and slowly-varying shift of the inertial sensors are effectively attenuated, and the system errors caused by scale factor instability, input axis misalignment and random white noise couldn't be attenuated. The error model of the dual-axis rotation-dwell inertial navigation system is designed in digital computer, and the theoretical conclusion is validated.
机译:捷联惯性导航系统(INS)的误差发散可以通过系统旋转自动补偿技术得到抑制。该技术可以有效地为系统带来更好的精度性能,而无需使用更高精度的陀螺仪和加速度计。介绍了一种八位置双轴旋转驻留方案,推导并分析了系统误差方程。通过实施此方案,某些错误的行为会发生变化。误差分析表明,由惯性传感器的恒定偏置和缓慢变化的位移引起的系统误差得到了有效的衰减,由比例因子的不稳定性,输入轴未对准和随机白噪声引起的系统误差无法得到衰减。在数字计算机上设计了双轴旋转停留惯性导航系统的误差模型,并验证了理论结论。

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