DocumentCode :
2048680
Title :
Autonomous attitude maneuver planning in asteroid exploration missions
Author :
Changqing Wu ; Rui Xu ; Shengying Zhu
Author_Institution :
Sch. of Aerosp. Eng., Beijing Inst. of Technol., Beijing, China
fYear :
2015
fDate :
2-5 Aug. 2015
Firstpage :
2290
Lastpage :
2295
Abstract :
During the asteroid exploration mission, attitude maneuver is subjected to various constraints, such as geometric constraints, dynamic constraints etc. To accomplish rapid maneuver from the initial attitude to the target attitude under the complex system constraints, autonomous attitude maneuver planning problem should be considered. This article fully considers the constraints in deep space environment, and describes the maneuver process in three-dimensional space to path planning in two-dimensional plane where the constraints are translated to some obstacles in this plane. To promote the attitude maneuver efficiency and decrease the time cost, an attitude path planning algorithm based on the genetic algorithm was proposed. Take the asteroid exploration mission Chang´e II as example, simulation results show that this method not only meets the previous constraints but also effectively gives the attitude maneuver path.
Keywords :
attitude control; genetic algorithms; path planning; space vehicles; Change II mission; asteroid exploration mission; attitude maneuver efficiency; attitude path planning algorithm; autonomous attitude maneuver planning; deep space environment; genetic algorithm; three-dimensional space; Angular velocity; Attitude control; Genetic algorithms; Path planning; Planning; Space vehicles; Sun; Asteroid explorer; Attitude control; Genetic algorithm; Path planning;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Mechatronics and Automation (ICMA), 2015 IEEE International Conference on
Conference_Location :
Beijing
Print_ISBN :
978-1-4799-7097-1
Type :
conf
DOI :
10.1109/ICMA.2015.7237843
Filename :
7237843
Link To Document :
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