DocumentCode :
3217375
Title :
Exploration Opportunity Search for Near Earth Small Body
Author :
Ren Yuan ; Cui Pingyuan ; Luan Enjie
Author_Institution :
Deep Space Exploration Center, Harbin Inst. of Technol., China
fYear :
2006
fDate :
7-11 Aug. 2006
Firstpage :
639
Lastpage :
643
Abstract :
Near-Earth object (NEO) exploration missions attract many scientists because asteroids and comets hold the key clues that could help us to understand the origin of the solar system and the formation of the planets. When selecting the target for a space mission, it requires trying to minimize the total velocity increment. Traditional "pork-chop" plot method exhausts the possible combination of launch time and arriving time to find the optimal exploration opportunity. In this paper, a novel search method based on the theory of transition matrix and calculus of variations is presented. This method firstly derive the analytical gradients of total velocity increment with respect to launch time and arriving time, and then a quasi-Newton method is utilized to search the optimal launch and arriving time under the drive of these analytical gradients. At the end of this paper, exploration opportunities of some NEOs with high scientific value are searched by the novel method. The novel method can find the exploration opportunity with low computational complexity, compared with "pork-chop" plot, and the precision of launch and arriving time could be increased easily.
Keywords :
Newton method; asteroids; comets; space research; space vehicles; asteroids; comets; computational complexity; near-Earth object exploration missions; planet formation; quasiNewton method; solar system origin; space mission; state transition matrix; total velocity increment; two-impulse transfer trajectory; variation calculus; Calculus; Computational complexity; Earth; Performance analysis; Planets; Solar system; Space exploration; Space missions; Space technology; Space vehicles; Calculus of variations; Pork-chop figure; State transition matrix; Two-impulse transfer trajectory;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference, 2006. CCC 2006. Chinese
Conference_Location :
Harbin
Print_ISBN :
7-81077-802-1
Type :
conf
DOI :
10.1109/CHICC.2006.280690
Filename :
4060599
Link To Document :
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