TY - GEN
T1 - The optimal guidance law for rendezvous and docking of spacecraft
AU - Zhu, Lingpu
AU - Liu, Zhenghua
AU - Wen, Nuan
N1 - Publisher Copyright:
© 2016 IEEE.
PY - 2017/1/20
Y1 - 2017/1/20
N2 - Rendezvous & docking (RVD) include four phases: ground longrang phase, homing phase, approach phase, docking phase. For the optimal rendezvous, most solutions are based on the C-W function. This paper studies the optimal rendezvous solutions which based on the traditional C-W equations, and studies optimal rendezvous solutions which based on the method of nonlinear programming. A recently developed direct optimization technique is employed, which converts the optimal control problem into a nonlinear programming one.
AB - Rendezvous & docking (RVD) include four phases: ground longrang phase, homing phase, approach phase, docking phase. For the optimal rendezvous, most solutions are based on the C-W function. This paper studies the optimal rendezvous solutions which based on the traditional C-W equations, and studies optimal rendezvous solutions which based on the method of nonlinear programming. A recently developed direct optimization technique is employed, which converts the optimal control problem into a nonlinear programming one.
KW - Nonlinear programming
KW - Optimal control
KW - Rendezvous & docking
KW - Spacecraft
UR - https://www.scopus.com/pages/publications/85015254098
U2 - 10.1109/CGNCC.2016.7828966
DO - 10.1109/CGNCC.2016.7828966
M3 - 会议稿件
AN - SCOPUS:85015254098
T3 - CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference
SP - 1243
EP - 1248
BT - CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016
Y2 - 12 August 2016 through 14 August 2016
ER -