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张国力, 纪元法, 孙希延. 用于导航姿态测量的改进人工蜂群算法J. 桂林电子科技大学学报, 2026, 46(1): 67-74. DOI: 10.16725/j.1673-808X.202425
引用本文: 张国力, 纪元法, 孙希延. 用于导航姿态测量的改进人工蜂群算法J. 桂林电子科技大学学报, 2026, 46(1): 67-74. DOI: 10.16725/j.1673-808X.202425
ZHANG Guoli, JI Yuanfa, SUN Xiyan. An enhanced artificial bee colony algorithm for navigation attitude measurementJ. Journal of Guilin University of Electronic Technology, 2026, 46(1): 67-74. DOI: 10.16725/j.1673-808X.202425
Citation: ZHANG Guoli, JI Yuanfa, SUN Xiyan. An enhanced artificial bee colony algorithm for navigation attitude measurementJ. Journal of Guilin University of Electronic Technology, 2026, 46(1): 67-74. DOI: 10.16725/j.1673-808X.202425

用于导航姿态测量的改进人工蜂群算法

An enhanced artificial bee colony algorithm for navigation attitude measurement

  • 摘要: 导航卫星姿态测量是借助卫星载波相位差分值得到基线的矢量描述,之后根据姿态求解算法计算载体的姿态信息。为了借助智能优化算法提高姿态角解算的精度,提出一种改进人工蜂群算法的姿态角解算算法。通过将2根基线矢量引入Wahba问题的求解过程中,构建姿态角的适应度函数模型,借助人工蜂群算法的整体框架,采用3D-CSCM混沌映射提升算法的初始遍历性,同时以天牛须搜索算法提升算法的收敛性能,最终搜索求解姿态角度值。通过对比实验验证,改进算法在105.588 1 m及47.047 3 m的基线长度下静态测量误差航向角为0.002 446°,俯仰角为0.001 654°,横滚角为0.006 808°,优于经典的SVD算法及QUEST算法,能够满足实时静态姿态求解的需求。

     

    Abstract: The attitude measurement of a navigation satellite is based on the vector description of the baseline with the phase difference of the satellite carrier, and then the attitude information of the carrier is calculated according to the attitude solving algorithm. In order to improve the accuracy of attitude Angle calculation with the help of an intelligent optimization algorithm, an attitude Angle calculation algorithm based on the artificial bee colony algorithm is proposed. By introducing two basic line vectors into the process of solving the Wahba problem, a fitness function model of attitude Angle is constructed. With the help of the overall framework of artificial bee colony algorithm, 3D-CSCM chaotic mapping is used to improve the initial ergodicity of the algorithm, and the beetle antennae search algorithm is used to improve the convergence performance of the algorithm. Finally, the attitude Angle value is searched and solved. Through comparative experiments, the static measurement error of the yaw algorithm is 0.002 446°, the pitch Angle is 0.001 654°, and the roll Angle is 0.006 808° at the baseline lengths of 105.588 1 m and 47.047 3 m, which is superior to the classical SVD algorithm and QUEST algorithm, and can meet the requirements of real-time static attitude solving.

     

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