一种非迭代的卫星导航PVT解算方法及其应用OA
A Non-iterative PVT Solution Method and Its Application for Satellite Navigation
卫星导航接收机进行位置、速度和时间(Position,Velocity,and Time,PVT)解算时,一般采用基于迭代的加权最小二乘方法.但由于该方法需进行多次迭代,运算量较大.为解决该问题,文章提出一种解决方案:首先,给出了一种非迭代的PVT解算方法,并提出先采用非迭代方法求解定位结果初值,然后再用传统迭代解算方法进行一次迭代解算的改进非迭代PVT解算方法;最后,利用DSP+FPGA架构的接收机进行了实物测试及验证.测试结果表明,该方法的解算精度与传统方法一致,但运算量降低了50%以上.
When the satellite navigation receiver solves the PVT(Position,Velocity,and Time),the Weighted Least Squares method based on iteration is generally used.However,due to the multiple iterations of this method,the amount of computation is large.In order to solve this problem,this paper proposes a solution.Firstly,a non-iterative PVT solution method is proposed,and an improved non-iterative PVT solution method is proposed to solve the initial value of the positioning result by using the non-iterative method.And then,it uses the traditional iterative solution method to perform an iterative solution.Finally,the receiver using DSP+FPGA architecture is tested and verified.The test results show that the solution accuracy of the proposed method is consistent with the traditional method,but the computational load is reduced by more than 50%.
辜永忠;邓恒淹;王功文;郑楷
成都天奥信息科技有限公司,四川 成都 611731成都天奥信息科技有限公司,四川 成都 611731成都天奥信息科技有限公司,四川 成都 611731成都天奥信息科技有限公司,四川 成都 611731
信息技术与安全科学
加权最小二乘非迭代PVT解算卫星导航DSP
Weighted Least Squaresnon-iterativePVT solutionsatellite navigationDSP
《现代信息科技》 2026 (5)
1-5,5
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