TY - JOUR
T1 - Optimal multiple-impulse rendezvous between non-coplanar elliptic orbits considering the J2 perturbation effects
AU - Zhou, Jun
AU - Chang, Yan
PY - 2008/3
Y1 - 2008/3
N2 - In this paper, the minimum-fuel, time-fixed optimal multiple-impulse rendezvous between non-coplanar elliptic orbits considering the J2 perturbation effects was mainly studied. Based on the perturbation theory, the kinetic equation of spacecraft rendezvous considering the J2 perturbation effects was deduced. The nonlinear programming model of optimal multi-impulse rendezvous was set up, and the optimization results of three-impulse and four-impulse were presented, the times, magnitudes and directions of optimal impulses were individually obtained. Finally, a great lot of simulations were done to investigate the fuel consumption with different time and impulses restraint.
AB - In this paper, the minimum-fuel, time-fixed optimal multiple-impulse rendezvous between non-coplanar elliptic orbits considering the J2 perturbation effects was mainly studied. Based on the perturbation theory, the kinetic equation of spacecraft rendezvous considering the J2 perturbation effects was deduced. The nonlinear programming model of optimal multi-impulse rendezvous was set up, and the optimization results of three-impulse and four-impulse were presented, the times, magnitudes and directions of optimal impulses were individually obtained. Finally, a great lot of simulations were done to investigate the fuel consumption with different time and impulses restraint.
KW - J2 perturbation
KW - Multiple-impulse maneuver
KW - Nonlinear programming
KW - Space rendezvous
KW - Trajectory optimization
UR - http://www.scopus.com/inward/record.url?scp=56849128815&partnerID=8YFLogxK
M3 - 文章
AN - SCOPUS:56849128815
SN - 1000-1328
VL - 29
SP - 472
EP - 475
JO - Yuhang Xuebao/Journal of Astronautics
JF - Yuhang Xuebao/Journal of Astronautics
IS - 2
ER -