Pseudospectral method based trajectory optimization and fairing rejection time analysis of solid launch vehicle
Tóm tắt
Từ khóa
Tài liệu tham khảo
Luo Y Z, Tang G J, Zhou L N. Hybrid genetic algorithm and its application on optimal ascend trajectory design of launch vehicle (in chinese). J Nation Univ Def Technol, 2004, 26(2): 5–8
John W H, Coverstone-Crroll V, Steven N W. Optimal interplanetary spacecraft trajectory via a Pareto genetic algorithm. J Astronaut Sci, 1998, 46(3): 267–282
Crain T P, Bishop R H, Fowler W T, et a1. Interplanetary fly by mission optimization using a hybrid global/local search method. J Spacecraft Rockets, 2000, 37(4): 468–473
Adam W, Tim C, Ellen B. Genetic algorithm and calculus of variations-based trajectory optimization technique. J Spacecraft Rockets, 2003, 40(6): 882–888
Ross I M, Fahroo F. Pseudospectral knotting methods for solving optimal control problems. J Guid Contr Dynam, 2004, 27(3): 397–405
Fahroo F, Ross I M. Costate estimation by a Legendre pseudospectral method. J Guid Contr Dynam, 2002, 24(2): 270–277
Fahroo F, Ross I M. Direct trajectory optimization by a Chebyshev pseudospectral method. J Guid Contr Dynam, 2002, 25(1): 160–166
Jia P R, Chen K J, He L. Ballistics of Long-distance Rocket (in chinese). Changsha: National University of Defense Technology Press, 1993. 57–58
Elnagar J, Kazemi M A, Razzaghi M. The pseudospectral Legendre method for discretizing optimal control problem. IEEE T Autom Contr, 1995, 40(10): 1793–1796
Elnagar J, Razzaghi M. A collocation-type method for linear quadratic optimal control problems. Optim Contr Appl Method, 1997, 18(3): 227–235
Gottlieb D, Hussaini M Y, Orszag S. Theory and Applications of Spectral Methods: Spectral Methods for PDE’s. Philadelphia: SIAM, 1987