GENETIC ALGORITHM APPROACH FOR OPTIMAL-CONTROL PROBLEMS WITH LINEARLY APPEARING CONTROLS

被引:31
作者
SEYWALD, H [1 ]
KUMAR, RR [1 ]
DESHPANDE, SM [1 ]
机构
[1] BOOZ ALLEN & HAMILTON INC, LOS ANGELES, CA 90086 USA
关键词
D O I
10.2514/3.56673
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
For optimal control problems in Mayer form with all controls appearing only Linearly in the equations of motion, this paper presents a method for calculating the optimal Solution without user-specified initial guesses and without a priori knowledge of the optimal switching structure. The solution is generated in a sequence of steps involving a genetic algorithm (GA), nonlinear programming, and (multiple) shooting, The centerpiece of this method is a variant of the GA that provides reliable initial guesses for the nonlinear programming method, even for large numbers of parameters. As a numerical example, minimum-time spacecraft reorientation trajectories are generated. The described procedure never failed to correctly determine the optimal solution.
引用
收藏
页码:177 / 182
页数:6
相关论文
共 16 条
  • [1] [Anonymous], 1989, GENETIC ALGORITHM SE
  • [2] Bartle R.G, 1975, ELEMENTS REAL ANAL, Vsecond
  • [3] Bell D. J., 1975, SINGULAR OPTIMAL CON
  • [4] BILIMORIA KD, 1990, MINIMUM TIME LARGE A
  • [5] BOCVAROV S, 1991, P AIAA GUIDANCE NAVI, P936
  • [6] Bryson A.E, 1975, APPL OPTIMAL CONTROL
  • [7] CHOWDHRY RS, 1990, AIAA9034585 PAP
  • [8] Gill P. E., 1981, PRACTICAL OPTIMIZATI
  • [9] GILL PE, USERS GUIDE NPSOL VE
  • [10] Goldberg D. E., 1992, Complex Systems, V6, P333