期刊文献+

炮射导弹控制系统的多目标二级优化设计

Design of Multi-Objective Bi-Level Optimization about the Control System of Gun-Launched Missile
下载PDF
导出
摘要 建立了炮射导弹多目标二级优化模型,提出了多目标二级混合遗传优化算法.对第一级多目标函数引入Lagrange乘子向量作为协调变量,采用两级递阶协调法实现多目标的第一级优化;针对遗传算法局部优化性能较差的缺点,将遗传算法与模式搜索法相结合,采用改进的遗传算法实现了多目标的第二级优化.仿真结果表明,所提出的多目标二级混合遗传优化算法收敛速度快,所设计的控制系统性能优于基于权重系数变换法的遗传算法的效果. Multi-objective bi-level optimization model for the control system of gun-launched missile is discussed. A bi-level hybrid genetic optimization algorithm for multi-objective is presented to solve the control of gun-launched missiles. First, by introduceing a Lagrange multiplier vector, the first-level model is optimized based on a hierarchical optimal. Then, combining the genetic algorithm to the pattern search, the second-level model is optimized. Simulation experiments showed that this hybrid genetic optimization algorithm, when compared to the known genetic algorithm, had {aster convergence and the optimized control system of the gun-launched missile can track the maneuvered acceleration more accurately and rapidly.
出处 《北京理工大学学报》 EI CAS CSCD 北大核心 2008年第10期875-879,共5页 Transactions of Beijing Institute of Technology
基金 国家部委预研项目(100502048)
关键词 导弹制导控制系统 多目标二级优化 混合遗传优化算法 guidance and control system of gun-launched missile multi-objective bi-level optimization hybrid genetic algorithm
  • 相关文献

参考文献10

二级参考文献35

  • 1孙晓燕,巩敦卫.变种群规模合作型协同进化遗传算法及其在优化中的应用[J].控制与决策,2004,19(12):1437-1440. 被引量:7
  • 2吴晓涛,孙增圻.用遗传算法进行路径规划[J].清华大学学报(自然科学版),1995,35(5):14-19. 被引量:75
  • 3Holland J. Adaptation in natural and artificial systems[M]. Ann Aror: University of Michigan Press, 1975.
  • 4Li Jianping. A species conserving genetic algorithm for multimodal function optimization[J ]. Evolutionary Coputation, 2002, 10(3): 207-234.
  • 5Passino K M. Fuzzy control[ M]. Mewlo Park: Addison Wesley Longrruan Inc, 1998.
  • 6周明.遗传算法及其应用[M].北京:电子工业出版社,1999..
  • 7Wise k A, Broy D J. Agile Missile Dynamics and Control [ J]. Journal of Guidance, Control and Dynamics, 1998,21 ( 3 ) :441 - 449.
  • 8Chadwick K A. Augmentation of High-altitude Maneuver Performance of Tail-controlled Missile Using Lateral Thrust[ R]. ADA-328973, 1997.
  • 9Yong S C, Choi C L, Jae W C. Autopilot Design for Agile Missile with Aerodynamic Fin and Side Thruster[ C].SICE Annual Conference, Fukui, Japan, 2003,1476-1481.
  • 10Menon P K, Iragavarapu V R. Adaptive Techniques for Multiple Actuator Blending[ C ]. AIAA Guidance, Navigation and Control Conference,Boston, MA, 1995.

共引文献47

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部