系统工程与电子技术

• 制导、导航与控制 • 上一篇    下一篇

无码载波频率初值估计与导航星识别

卢欢1, 郁丰2, 刘莹3, 朱海微2   

  1. 1.南京航空航天大学自动化学院, 江苏 南京 210016; 2. 南京航空航天大学航天学院,
    江苏 南京 210016; 3. 上海卫星工程研究所, 上海 200240
  • 出版日期:2016-09-28 发布日期:2010-01-03

Codeless carrier frequency initial value estimation and#br# navigation satellite recognition

LU Huan1, YU Feng2, LIU Ying3, ZHU Hai-wei2   

  1. 1.College of Automation Engineering, Nanjing University of Aeronautics & Astronautics,
    Nanjing 210016, China; 2. College of Astronautics, Nanjing University of Aeronautics & Astronautics,
    Nanjing 210016, China;3.Shanghai Institute of Satellite Engineering, Shanghai 200240, China
  • Online:2016-09-28 Published:2010-01-03

摘要:

当导航卫星的民码信号不可用时,利用无码载波恢复技术测量各个导航卫星的多普勒频移能够实现多普勒定轨。针对伪码未知的情况,提出了基于相位补偿及数据块累加来增强信号,并结合快速傅里叶变换估计载波频率的方法;为解决无码条件下的导航卫星识别问题,提出了一种基于多普勒频移特征的导航星识别方法,研究了基于三分法快速搜索优化平移量的匹配算法,并采用全局匹配、局部剔除的策略来提高卫星识别的全局可信度。仿真结果表明,对于80 ms的卫星中频数据,无码载波频率估计误差保持在7 Hz之内,并且正确估计的卫星数在9颗以上;在考虑先验参数不精准及测量误差的情况下,正确识别的卫星数大多为6颗及以上,满足定轨要求的最少卫星数目。

Abstract:

There is a way of Doppler orbit determination that recovers carrier signal effectively, and measures the Doppler frequency shift precisely when civil codes of satellite navigation signals are not available. For unknown pseudo-code, a method based on phase compensation and data block accumulation is presented to estimate the carrier frequency of the square signal accurately. For codeless navigation satellite identification, a method based on the characteristics of Doppler frequency shift is proposed, and the clock frequency offset of the receiver is received,and the match algorithm based on the three points method is researched. The global match, local elimination strategy is adopt to improve the reliability of satellite recognition. The simulation reveals that codeless carrier frequency estimation error is within 7 Hz, and the number of satellites estimated correctly is 9 or more. Considering the inaccuracy prior parameters and measurement errors, at least 6 satellites are identified correctly, which satisfies the requirement of orbit determination of satellites.