DocumentCode :
3056946
Title :
Research on optimal strategy of fixed-time rendezvous
Author :
Tan, Lifen ; Yan, Ye ; Zhou, Ying ; Tang, Guojin
Author_Institution :
Coll. of Aerosp. & Mater. Eng., Nat. Univ. of Defense Technol., Changsha, China
fYear :
2010
fDate :
8-10 June 2010
Firstpage :
1065
Lastpage :
1069
Abstract :
Fuel optimization of fixed time hard rendezvous problem is studied. Optimal fuel is calculated by indirect and direct approaches respectively. The indirect approach is based on primer vector theory, and primer vector of transfer orbit is calculated and improved. A nonlinear optimization model is formulated for the problem of multiple-impulse rendezvous optimizing by direct approach, and the optimal number of impulses, their times and magnitude are obtained numerically. Finally, the optimal transfer strategy for studied type of rendezvous problem is put forward.
Keywords :
aircraft control; nonlinear control systems; optimal control; optimisation; fixed time hard rendezvous; fixed-time rendezvous; fuel optimization; multiple-impulse rendezvous; nonlinear optimization model; optimal fuel; optimal strategy; optimal transfer strategy; primer vector theory; transfer orbit; History; Mathematical model; Optimization; Orbits; Simulation; Space vehicles; Trajectory;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on
Conference_Location :
Harbin
Print_ISBN :
978-1-4244-6043-4
Electronic_ISBN :
978-1-4244-7505-6
Type :
conf
DOI :
10.1109/ISSCAA.2010.5634036
Filename :
5634036
Link To Document :
بازگشت