TY - GEN
T1 - Exploration opportunity search for near earth small body
AU - Ren, Yuan
AU - Cui, Pingyuan
AU - Luan, Enjie
PY - 2006
Y1 - 2006
N2 - 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.
AB - 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.
KW - Calculus of variations
KW - Pork-chop figure
KW - State transition matrix
KW - Two-impulse transfer trajectory
UR - http://www.scopus.com/inward/record.url?scp=37348999552&partnerID=8YFLogxK
U2 - 10.1109/CHICC.2006.280690
DO - 10.1109/CHICC.2006.280690
M3 - Conference contribution
AN - SCOPUS:37348999552
SN - 7810778021
SN - 9787810778022
T3 - 2006 Chinese Control Conference Proceedings, CCC 2006
SP - 639
EP - 643
BT - 2006 Chinese Control Conference Proceedings, CCC 2006
PB - IEEE Computer Society
T2 - 25th Chinese Control Conference, CCC 2006
Y2 - 7 August 2006 through 11 August 2006
ER -