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逆向导航算法及其在捷联罗经动基座初始对准中的应用

Study on reverse navigation algorithm and it’s application to SINS gyrocompass in-movement alignment

中文摘要英文摘要

根据捷联惯导系统的导航更新算法,推导了逆向导航算法。提出了捷联罗经动基座初始对准方案,它包括三个阶段:方位角未知情况下水平对准、粗略方位自对准和罗经方位对准。在导航计算机存储容量足够大并且计算能力足够强的条件下,通过逆向导航算法将动基座初始对准与位置导航结合起来,先进行捷联罗经动基座初始对准和传感器采样数据存储,再利用逆向航位推算算法和正向航位推算算法,同时实现初始对准和位置导航。最后利用车载试验验证了所提方法的有效性,在运动条件下经过10分钟,方位对准达到0.112º(1σ)、位置导航精度约0.1%×行驶路程。

Reverse navigation algorithms are deduced based on the classical strapdown inertial navigation system (SINS) updating algorithms. The scheme of SINS gyrocompass in-movement alignment is proposed and is divided into three steps, including leveling alignment with header uncertainty, coarse header alignment and gyrocompass alignment for header. On the assumption of navigation computer having large memory and powerful computing ability, the connection between in-movement alignment and vehicle position navigation are established by reverse navigation algorithm. After the process of SINS gyrocompass in-movement alignment and saving sensor’s samples to memory, reverse and normal dead reckoning algorithm are executed in succession to accomplish vehicle position updating. Finally, some vehicular tests prove that the proposed alignment algorithm in this paper is effective. In move base, the alignment accuracy of header reaches 0.112º(1σ) and the accuracy of position updating is about 0.1% by distance.

严卫生、严恭敏、徐德民

航空航天技术自动化技术、自动化技术设备

捷联惯导系统,逆向导航,动基座初始对准,罗经,航位推算

strapdown inertial navigation systemreverse navigationin movement alignmentgyrocompassdead reckoning

严卫生,严恭敏,徐德民.逆向导航算法及其在捷联罗经动基座初始对准中的应用[EB/OL].(2007-10-31)[2025-08-11].http://www.paper.edu.cn/releasepaper/content/200710-575.点此复制

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