基于星地差分GPS的航天测控系统在线误差标校方法研究

王瞧; 金小军; 张伟; 莫仕明; 徐兆斌; 金仲和

doi:10.1631/FITEE.1800308

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基于星地差分GPS的航天测控系统在线误差标校方法研究

常规文章 | Updated：2022-05-19

- 基于星地差分GPS的航天测控系统在线误差标校方法研究
- An online error calibration method for spaceflight TT & C systems based on LEO-ground DDGPS
- 信息与电子工程前沿（英文） 2019年20卷第6期页码：829-841
- Affiliations：
  
  Micro-Satellite Research Center, Zhejiang University, Hangzhou 310027, China
- Author bio：
  
  [ "Qiao WANG, E-mail: wqiao2010@zju.edu.cn" ]
  Xiao-jun JIN, E-mail: axemaster@zju.edu.cn
- Funds：
  
  Project supported by the National Natural Science Foundation of China (Nos. 60904090 and 61401389), the National Science Foundation for Distinguished Young Scholars of China (No. 61525403), the Joint Fund of the Ministry of Education of China (No. 6141A02033310), and the Fundamental Research Funds for the Central Universities, China (No. 2018QNA4053)
- DOI：10.1631/FITEE.1800308
  中图分类号： TP39;V19
- 收稿：2018-05-19，
  
  修回：2019-;6-11，
  
  纸质出版：2019-06
- Accepted：
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王瞧, 金小军, 张伟, 等. 基于星地差分GPS的航天测控系统在线误差标校方法研究[J]. 信息与电子工程前沿（英文）, 2019,20(6):829-841.

Qiao WANG, Xiao-jun JIN, Wei ZHANG, et al. An online error calibration method for spaceflight TT & C systems based on LEO-ground DDGPS[J]. Frontiers of Information Technology & Electronic Engineering, 2019, 20(6): 829-841.
王瞧, 金小军, 张伟, 等. 基于星地差分GPS的航天测控系统在线误差标校方法研究[J]. 信息与电子工程前沿（英文）, 2019,20(6):829-841. DOI： 10.1631/FITEE.1800308.

Qiao WANG, Xiao-jun JIN, Wei ZHANG, et al. An online error calibration method for spaceflight TT & C systems based on LEO-ground DDGPS[J]. Frontiers of Information Technology & Electronic Engineering, 2019, 20(6): 829-841. DOI： 10.1631/FITEE.1800308.

摘要

为克服传统误差标校方法的缺点，提出一种基于星地差分GPS的航天测控系统在线误差标校方法。该方法采用固定区间平滑算法，平滑前向、后向抗差自适应卡尔曼滤波结果，同时基于蚁群最优化算法固定星地差分GPS载波相位模糊度，以获取高精度星地基线测量结果。将该结果作为航天测控系统比较标准，并用最小二乘批处理算法求解测距误差模型。利用Spirent导航信号模拟器和自主研制的星载GPS双频接收机，构建半实物仿真平台对该误差标校方法进行仿真验证。结果表明，固定区间平滑算法平滑后，星地基线解算精度（RMS，单轴）优于10 cm。测距系统误差标定后，残差优于5 cm。

Abstract

To overcome the shortcomings of the traditional measurement error calibration methods for spaceflight telemetry

tracking and command (TT & C) systems

an online error calibration method based on low Earth orbit satellite-to-ground double- differential GPS (LEO-ground DDGPS) is proposed in this study. A fixed-interval smoother combined with a pair of forward and backward adaptive robust Kalman filters (ARKFs) is adopted to solve the LEO-ground baseline

and the ant colony optimization (ACO) algorithm is used to deal with the ambiguity resolution problem. The precise baseline solution of DDGPS is then used as a comparative reference to calibrate the systematic errors in the TT & C measurements

in which the parameters of the range error model are solved by a batch least squares algorithm. To validate the performance of the new online error calibration method

a hardware-in-the-loop simulation platform is constructed with independently developed spaceborne dual-frequency GPS receivers and a Spirent GPS signal generator. The simulation results show that with the fixed-interval smoother

a baseline estimation accuracy (RMS

single axis) of better than 10 cm is achieved. Using this DDGPS solution as the reference

the systematic error of the TT & C ranging system is effectively calibrated

and the residual systematic error is less than 5 cm.

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