Optimization of multiple-impulse minimum-time rendezvous with impulse constraints using a hybrid genetic algorithm

Aerospace Science and Technology

Volumn 10, Issue 6, 2006, Pages 534-540

  Luo, Ya Zhong ^a   Tang, Guo Jin ^a   Li, Hai yang ^a  

^a NATIONAL UNIVERSITY OF DEFENSE TECHNOLOGY   (China)

Author keywords

Genetic algorithm; Global optimization; Impulse constraints; Minimum time; Multiple impulse rendezvous

Indexed keywords

ALGORITHMS; CONSTRAINT THEORY; GENETIC ALGORITHMS; GLOBAL OPTIMIZATION; LINEAR EQUATIONS; MATHEMATICAL MODELS;

IMPULSE CONSTRAINTS; MINIMUM-TIME; MULTIPLE-IMPULSE RENDEZVOUS;

SPACE RENDEZVOUS;

EID: 33748301985     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2005.12.007     Document Type: Article

References (25)

1. Anderson M.B., Burkhalter J.E., and Jenkins R.M. Design of a guided missile interceptor using a genetic algorithm. J. Spacecraft and Rockets 38 1 (2001) 28-35
2. Betts J.T. Survey of numerical methods for trajectory optimization. J. Guidance Control Dynam. 21 2 (1998) 193-207
3. Carter T.E., and Alvarez S.A. Quadratic-based computation of four-impulse optimal rendezvous near circular orbit. J. Guidance Control Dynam. 23 1 (2000) 109-117
4. Clohessy W.H., and Wiltshire R.S. Terminal guidance system for satellite rendezvous. J. Aerospace Sci. 27 9 (1960) 653-658
5. Crain T., Bishop R.H., and Fowler W. Interplanetary flyby mission optimization using a hybrid global-local search method. J. Spacecraft and Rockets 37 4 (2000) 468-474
6. P.E. Gill, W. Murray, M.A. Saunders, M.A. Wright, User's guide to NPSOL 5.0, A Fortran package for nonlinear programming, Standford Optimization Lab., Stanford Univ., TR SOL 86-1, CA, July 1998
7. Goldberg D.E. Genetic Algorithms in Search, Optimization and Machine Learning (1989), Addison Wesley Longman, Reading, MA
8. Gross L.R., and Prussing J.E. Optimal multiple-impulse direct ascent fixed-time rendezvous. AIAA J. 12 7 (1974) 885-889
9. Hajela P. Soft computing in multidisciplinary aerospace design-new directions for research. Progr. Aerospace Sci. 38 (2002) 1-22
10. Hughes G.W., and McInnes C.R. Solar sail hybrid trajectory optimization for non-Keplerian orbit transfers. J. Guidance Control Dynam. 25 3 (2002) 602-604
11. Jones J.B. Optimal rendezvous in the neighborhood of a circular orbit. J. Astronautical Sci. 24 1 (1976) 55-90
12. Kechichian J.A. The algorithm of the two-impulse time-fixed noncoplanar rendezvous with drag and oblateness effects. J. Astronautical Sci. 46 1 (1998) 47-64
13. Kim Y.H., and Spencer D.B. Optimal spacecraft rendezvous using genetic algorithms. J. Spacecraft and Rockets 39 6 (2002) 859-865
14. Luo Y.Z., Tang G.J., and Liang Y.G. Decomposition approach and genetic algorithm based global optimization of launch trajectory for sun synchronous orbit. Chinese J. Aeronautica 25 5 (2004) 443-446 (in Chinese)
15. Michalewicz Z., Janikow C., and Krawczyk J. A modified genetic algorithm for optimal control problem. Comput. Math. Appl. 23 2 (1992) 83-94
16. Nelder J.A., and Mead R. A simplex method for function minimization. Comput. J. 7 (1965) 308-313
17. Powell M.J.D. An efficient method for finding the minimum of a function of several variables without calculating derivatives. Computer J. 7 (1965) 303-307
18. Prussing J.E. Optimal four-impulse fixed-time rendezvous in the vicinity of a circular orbit. AIAA J. 7 5 (1969) 928-935
19. Prussing J.E. Optimal two- and three-impulse fixed-time rendezvous in the vicinity of a circular orbit. AIAA J. 8 7 (1970) 1221-1228
20. Prussing J.E., and Chiu J.H. Optimal multiple-impulse time-fixed rendezvous between circular orbits. J. Guidance Control Dynam. 9 1 (1986) 17-22
21. Prussing J.E. A class of optimal two-impulse rendezvous using multiple-revolution Lambert solutions. J. Astronautical Sci. 48 2 (2000) 131-148
22. Shen H.J., and Tsiotras P. Optimal two-impulse rendezvous using multiple-revolution Lambert solutions. J. Guidance Control Dynam. 26 1 (2003) 50-61
23. Taur D.R., Coverstone-Carrol V., and Prussing J.E. Optimal impulse time-fixed orbital rendezvous and interception with path constraints. J. Guidance Control Dynam. 18 1 (1995) 54-60
24. Xiang K.H., and Xiao Y.L. A study of propellant consumption of impulsive maneuvers in space rendezvous. Chinese J. Space Sci. Technol. 19 3 (1999) 9-15 (in Chinese)
25. Yokoyama N., and Suzuki S. Modified genetic algorithm for constrained trajectory optimization. J. Guidance Control Dynam. 28 1 (2005) 139-144