DocumentCode
2001399
Title
Solving orbit maintenance problems by the synthesis of evolution algorithms and traditional optimization methods
Author
Wang, Shi ; Liao, Shouyi ; Dai, Jinhai
Author_Institution
Coll. of Astronaut. & Material Eng., Nat. Univ. of Defense Technol., Changsha, China
Volume
2
fYear
2002
fDate
2002
Firstpage
1404
Abstract
Orbit maintenance problems are solved by the synthesis of the traditional penalty function method and evolution algorithms (EAs). A general method is presented for the n-time impulse problem of orbit maintenance. The algorithm is proved to be effective according to a simulation example which adjusts the semi-major axis with 3,4,5 impulse times.
Keywords
aerospace control; artificial satellites; convergence; evolutionary computation; optimisation; evolutionary algorithms; n-time impulse problem; orbit maintenance problems; semi-major axis adjustment; traditional optimization methods; traditional penalty function method; Algebra; Constraint optimization; Control systems; Educational institutions; Engines; Mathematics; Optimization methods; Satellites; Space missions; Space technology;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Control and Automation, 2002. Proceedings of the 4th World Congress on
Print_ISBN
0-7803-7268-9
Type
conf
DOI
10.1109/WCICA.2002.1020812
Filename
1020812
Link To Document