Observability analysis of satellite autonomous orbit determination with modeling and measurement errors

doi:10.16708/j.cnki.1000-758X.2023.0035

Abstract

Abstract: Autonomous orbit determination for a satellite with modelling and measurement errors is concerned in this paper．It’s well known that the performance of autonomous orbit determination is greatly affected by systematic errors in the dynamic model and the measurement.One way to deal with these errors is treating them as unknown biases and estimating them with dynamic states of the satellite together.Based on k-order local weak observability theory，sufficient and necessary conditions of k-order local weak observability were mathematically proved for the orbit determination system with these errors.The extended Kalman filter was applied to estimate orbital states and these systematic errors simultaneously．Simulation results show that the estimation algorithm is effective when the modeling errors and measurement errors are constant or slow time-varying for non-circular orbits.

Key words: orbit determination, modeling error, measurement error, autonomous navigation, observability analysis, nonlinear systems

ZHOU Bochao, LI Yong, ZHANG Ai, CUI Shihang. Observability analysis of satellite autonomous orbit determination with modeling and measurement errors[J]. Chinese Space Science and Technology, 2023, 43(3): 25-34.

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URL: https://journal26.magtechjournal.com/kjkxjs/EN/10.16708/j.cnki.1000-758X.2023.0035

https://journal26.magtechjournal.com/kjkxjs/EN/Y2023/V43/I3/25

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[2]	ZHOU Bochao, LI Yong. A multi-stage filter for autonomous navigation of formation satellites based on inter-satellite measurements [J]. Chinese Space Science and Technology, 2022, 42(3): 124-131.
[3]	LIU Siyu, HUANG Yong, MAO Yindun, JIA Yaohong, LU Wenqiang, HUANG Chengli, ZHENG Jinghui, YANG Peng. Precise orbit determination of FY-4 synchronous orbit satellite based on optical angle measurement data [J]. Chinese Space Science and Technology, 2021, 41(6): 54-62.
[4]	DING Taowei, SHUAI Ping, HUANG Liangwei, ZHANG Xinyuan. An autonomous orbit determination algorithm of XPNAV-1 based on extended Kalman filtering [J]. Chinese Space Science and Technology, 2021, 41(1): 13-21.
[5]	YE Zipeng, ZHOU Qingrui, WANG Hui. Research on autonomous navigation method for deep space exploration spacecraft in cruise phase [J]. Chinese Space Science and Technology, 2020, 40(5): 53-60.
[6]	ZHANG Zhibin, WANG Wei, YANG Peng, KALIUZHNYI Mykolay, MI Ligong, LI Guanghui, LI Peng, TANG Zhenghong, CUI Lang, HUANG Yong, WANG Guangli. Micro VLBI network for GEO satellite monitoring [J]. Chinese Space Science and Technology, 2020, 40(5): 119-125.
[7]	TANG Qingyuan, WANG Xiaolei. Autonomous navigation based on Deimos lightofsight for Mars approaching phase [J]. Chinese Space Science and Technology, 2019, 39(6): 38-.
[8]	DENG Guanghui, LIAO Zhuofan, ZHU Rong, WANG Jiongqi. Spacecraft autonomous navigation with cubature Kalman filter based on sun-earth-moon information#br# [J]. Chinese Space Science and Technology, 2018, 38(1): 70-76.
[9]	WANG Da-Bao, WANG Zhong-Guo, TANG Hai-Tao, CAO Jing. GPS Based Orbit Determination Algorithm with High Precisionand Low Computational Complexity for LEO Remote Sensing Satellites [J]. Chinese Space Science and Technology, 2014, 34(2): 54-61.
[10]	DANG Jian-Jun, LUO Jian-Jun, WAN Yan-Hui. Method of On-orbit Calibrating Scale Factor of Accelerometer Based on Lever Arm Effect [J]. Chinese Space Science and Technology, 2013, 33(2): 19-24.
[11]	GUO Xiang, ZHANG Qiang, ZHAO Qi-Le, GUO Jing. Precise Orbit Determination for LEO Satellites Using Single-frequency GPS Observations [J]. Chinese Space Science and Technology, 2013, 33(2): 41-46.
[12]	SHI Heng, XU Shi-Jie. Autonomous Navigation and In-orbit Parameter Calibration for Continuous Low Thrust Spacecraft [J]. Chinese Space Science and Technology, 2012, 32(4): 62-70.
[13]	CHEN Zhi-Guo, CHEN Pei, HAN Chao. Algorithm for Ground-base Orbit Determination of Navigation Satellites [J]. Chinese Space Science and Technology, 2012, 32(3): 27-34.
[14]	FU Juan, CHEN Xiao-Qian, HUANG Yi-Yong. Compression Mass Gauge Method for Liquid Propellant Residue [J]. Chinese Space Science and Technology, 2012, 32(3): 78-83.
[15]	LUO Nan, XU Lu-Ping, ZHANG Hua. Method of Autonomous Celestial Navigation Based on UKF and Information Fusion [J]. Chinese Space Science and Technology, 2012, 32(2): 1-9.

Observability analysis of satellite autonomous orbit determination with modeling and measurement errors

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