Journal of Systems Engineering and Electronics ›› 2010, Vol. 32 ›› Issue (9): 1951-1956.doi: 10.3969/j.issn.1001-506X.2010.09.35

• 制导、导航与控制 • 上一篇    下一篇

再入机动飞行器最优轨迹设计与跟踪

李海军,黄显林,葛东明   

  1. 哈尔滨工业大学控制理论与制导技术研究中心, 黑龙江 哈尔滨 150001
  • 出版日期:2010-09-06 发布日期:2010-01-03

Optimal trajectory design and tracking for maneuver reentry vehicles

LI Hai-jun,HUANG Xian-lin,GE Dong-ming   

  1. Center for Control Theory and Guidance Technology, Harbin Inst. of Technology, Harbin 150001, China
  • Online:2010-09-06 Published:2010-01-03

摘要:

提出了一种再入机动飞行器(maneuvering reentry vehicle, MRV)的最优制导与控制方案。针对MRV再入机动轨迹优化问题,提出了新的基于Gauss伪谱优化方法的分段优化策略;由产生的最优参考轨迹,生成系统的外环最优制导指令。接着利用轨迹线性化控制(trajectory linearization control, TLC)方法设计系统的内环控制律。基于MRV完整的非线性六自由度模型,仿真表明提出的再入轨迹优化设计方法是有效的,而且内环TLC控制器可以准确地跟踪外环的最优制导指令和最优轨迹,并对系统未建模特性和参数不确定性具有一定的鲁棒性能。

Abstract:

An optimal guidance and control architecture for a maneuvering reentry vehicle (MRV) is proposed. Based on the Gauss pseudospectrum method, a new multi-phases optimization strategy is proposed to deal with the difficulties in the optimization of maneuvering trajectory for MRV. Out-loop optimal guidance commands are generated from the resulted optimal reference trajectory. The inner-loop control law is designed based on the trajectory linearization control (TLC) method. Using the full nonlinear six degree-of-freedom model of the MRV, the simulation results show that the trajectory optimization method is effective, and the TLC controller of the inner-loop is able to track the maneuver command and the optimized trajectory accurately and robustly in the presence of unmodeled dynamics and parametric uncertainties.