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长航时捷联惯导重力扰动影响及补偿
Analysis and compensation of disturbing gravity effect on long-endurance strap-down inertial navigation system
【摘要】 从捷联惯导系统导航解算出发,分析了重力扰动矢量对捷联惯导误差的影响,并根据非均匀B样条最小二乘法,对局部区域内的重力扰动进行二维逼近,建立重力扰动模型,进而对捷联惯导系统进行补偿。仿真结果表明,非均匀B样条建模方法具有很好的精度,利用建立的重力扰动模型对长航时捷联惯导进行补偿可以有效地减小惯导误差。
【Abstract】 The effect of disturbing gravity vector on Strap-down Inertial Navigation System(SINS)errors is analyzed from the navigation calculation aspects. Then disturbing gravity model is established using the non-uniform B-spline least squares technology which can compensate for SINS. Simulation results show that the gravity modeling method has good precision, and the compensation for long-endurance SINS based on gravity model can reduce the SINS errors effectively.
【关键词】 捷联惯导系统;
重力扰动;
补偿;
【Key words】 strap-down inertial navigation system; disturbing gravity; compensation;
【Key words】 strap-down inertial navigation system; disturbing gravity; compensation;
【基金】 国家部委预研基金
- 【文献出处】 计算机工程与应用 ,Computer Engineering and Applications , 编辑部邮箱 ,2014年11期
- 【分类号】P227.9
- 【被引频次】2
- 【下载频次】132