导弹与制导技术

高动态条件下的捷联惯导并行算法研究

  • 林灿龙 ,
  • 马龙华 ,
  • 吴铁军 ,
  • 冯琼华
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  • 1 浙江大学控制科学与工程学系, 杭州 310027
    2 浙江大学导航制导与控制研究所, 杭州 310027

林灿龙(1986-),男,山东汕头人,硕士研究生,研究方向:捷联惯导算法并行化。

收稿日期: 2011-06-21

  网络出版日期: 2025-05-29

基金资助

国家自然科学基金(61070003);浙江省自然科学基金(R1090052)

Research of Parallel Strapdown Inertial Navigation Algorithm for High Dynamic Conditions

  • LIN Canlong ,
  • MA Longhua ,
  • WU Tiejun ,
  • FENG Qionghua
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  • 1 Department of Control Science and Engineering, Zhejiang University, Hangzhou 310027, China
    2 Institute of Navigation, Guidance and Control, Zhejiang University, Hangzhou 310027, China

Received date: 2011-06-21

  Online published: 2025-05-29

摘要

为提高高动态条件下导航解算的速度,文中给出了一种单更新速率的并行导航解算算法。该并行算法由并行姿态算法模块、并行速度算法模块、并行位置算法模块和参数计算模块等4个并行执行的模块组成。分析表明,该并行算法的总执行周期仅为普通算法的6%左右,显著提高了计算速度。基于FPGA的仿真实验结果表明,这一设计可大大提高导航解算算法的更新速率,对在高动态条件下提高导航解算的精度有重要作用。

本文引用格式

林灿龙 , 马龙华 , 吴铁军 , 冯琼华 . 高动态条件下的捷联惯导并行算法研究[J]. 弹箭与制导学报, 2012 , 32(2) : 1 -5,10 . DOI: 10.15892/j.cnki.djzdxb.2012.02.016

Abstract

A parallel navigation computation algorithm with a single update frequency was proposed and analyzed to increase the navigation computation updating rate in high dynamic conditions. The parallel algorithm includes 4 parallel computation modules: the parallel attitude computation module, the parallel velocity computation module, the parallel position computation module, and the parallel parameter computation module. The computation speed analysis shows that the total implement periods of the parallel algorithm are about 6% of conventional algorithms. The results of FPGA-based experiment show that the design significantly increases the updating rate of the navigation computation, thus greatly benefiting the navigation accuracy in high dynamic conditions.

参考文献

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