DocumentCode :
1795346
Title :
Design and stationkeeping of Lissajous trajectories about the Earth-Moon collinear libration points
Author :
Liu Lei ; Cao Jian-feng
Author_Institution :
Sci. & Technol. on Aerosp. Flight Dynamics Lab., Beijing Aerosp. Control Center, Beijing, China
fYear :
2014
fDate :
8-10 Aug. 2014
Firstpage :
2439
Lastpage :
2442
Abstract :
Lissajous trajectories about the collinear libration points are relevant on the space environment and deep space exploration, but have complex kinetic characteristics in the nature, thus their design and stationkeeping have always been focused in the deep space navigation and control field. This paper explores orbit design and maintenance technology of the Lissajous trajectories about the collinear Earth-Moon libration points under the real dynamical conditions. First, based on the restricted three body problem, the mathematic model of Lissajous orbit design and control with the real dynamical model was analyzed. The continue-circling method was presented for the Lissajous orbit design and control. Then the Lissajous trajectories about Earth-Moon collinear libration point was designed under the nature environment, and the third-body gravitation and the solar radiation pressure perturbations and their level were studied, and their impact on the Lissajous orbit stability was analyzed. Finally, based on the perturbation impact and stability analysis and orbit tracking and control frequency, this paper framed a stationkeeping strategy for the Lissajous orbit about the Earth-Moon collinear libration points. This paper can provide a reference for the future Lissajous orbit mission.
Keywords :
aerospace instrumentation; space vehicles; Earth-Moon collinear libration points; Lissajous orbit design; Lissajous orbit stability; Lissajous trajectories stationkeeping; continue-circling method; control frequency; deep space exploration; orbit tracking; solar radiation pressure perturbations; space environment; stability analysis; third-body gravitation; Maintenance engineering; Mathematical model; Moon; Orbits; Space vehicles; Stability analysis; Trajectory; Earth-Moon Collinear libration; Lissajous orbit; Restricted three body problem; orbit design; orbit maintenance;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
Conference_Location :
Yantai
Print_ISBN :
978-1-4799-4700-3
Type :
conf
DOI :
10.1109/CGNCC.2014.7007552
Filename :
7007552
Link To Document :
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