Satellite Attitude Determination Using ADS-B Receiver and MEMS Gyro

被引:6
作者
Liu, Zhiyong [1 ]
Zhou, Kaixing [2 ]
Sun, Xiucong [3 ]
机构
[1] Wuhan Univ, Sch Remote Sensing & Informat Engn, Wuhan 430072, Peoples R China
[2] Beijing Inst Elect Syst Engn, Beijing 100854, Peoples R China
[3] Beihang Univ, Sch Astronaut, Beijing 100191, Peoples R China
关键词
ADS-B; gyro; attitude determination; QUEST; NLSE; MEKF;
D O I
10.3390/aerospace10040370
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Automatic dependent surveillance-broadcast (ADS-B) is a very important communication and surveillance technology in air traffic control (ATC). In the future, more and more satellites will carry out ADS-B technology to perform a global coverage. In order to make full use of the resources in the satellite, this paper proposes a solution for satellite three-axis attitude determination using the ADS-B receiver. The principle of ADS-B-based attitude determination is presented first. On this basis, ADS-B-based methods are employed to solve the problem. To achieve a higher attitude determination precision, gyro is combined with the ADS-B receiver using a multiplicative extended Kalman filter (MEKF). Finally, a simulation is carried out and the result is presented.
引用
收藏
页数:20
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