DocumentCode :
2077978
Title :
Space Relative Navigation Filter Based On-Board Radar Observation
Author :
Ma, Weihua ; Luo, Jianjun ; Wang, Mingming ; Yang, Bo
Author_Institution :
Coll. of Astronaut., Northwestern Polytech. Univ., Xi´´an, China
fYear :
2009
fDate :
17-19 Oct. 2009
Firstpage :
1
Lastpage :
5
Abstract :
The absolute attitude error of chaser vehicle is always neglected in observation equation of space relative navigation filter when chaser satellite on-board radar using as the measurement sensor. But the attitude error could affect relative navigation filter precision in fact. The new observation equation, which contains the absolute attitude error of chaser vehicle, is constructed. And the plan, using equivalent measurement error as attitude error, is put forward. The simulations show that the filter precision of relative position and velocity descend when attitude error is big, and the precision is improved when attitude equivalent error is introduced to filter. The plan of attitude equivalent error is proved to be feasible.
Keywords :
aircraft navigation; attitude measurement; measurement errors; spaceborne radar; absolute attitude error; chaser satellite on-board; chaser vehicle; equivalent measurement error; measurement sensor; on-board radar observation; space relative navigation filter; Equations; Extraterrestrial measurements; Jacobian matrices; Laser radar; Measurement errors; Microwave filters; Radar measurements; Satellite navigation systems; Spaceborne radar; Vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Image and Signal Processing, 2009. CISP '09. 2nd International Congress on
Conference_Location :
Tianjin
Print_ISBN :
978-1-4244-4129-7
Electronic_ISBN :
978-1-4244-4131-0
Type :
conf
DOI :
10.1109/CISP.2009.5301217
Filename :
5301217
Link To Document :
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