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采用TLC方法的超机动飞行控制系统设计 被引量：6

Super-Maneuverable Flight Control System Based on TLC Method
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摘要 基于轨迹线性化控制(Trajectory linearization control,TLC)方法,研究了超机动飞机飞行控制系统的设计问题。首先简要介绍了TLC方法的设计思想;然后根据奇异摄动理论,将超机动飞行控制系统分成快慢两个回路,并为其分别设计了轨迹线性化控制器;最后分别用所设计的控制器和已有的动态逆控制器对某型歼击机进行了赫布斯特机动仿真。仿真结果和对比分析表明,所设计的TLC控制器是有效的,且比动态逆控制器具有更好的控制跟踪性能。 A control law based on trajectory linearization control （TLC） method is designed and implemented. Firstly, the design principle of TLC is introduced. Then based on the singular perturbation theory, the super-maneuverable flight control system is divided into two loops： fast loop. and slow loop, and TLC controllers are designed. Finally, Herbst maneuver is simulated for super-maneuverable aircrafts using a TLC controller. For comparison, under the same condition, the herbst maneuver is also simulated using a dynamic-inversion controller. Simulation results show that the TLC controller is effective and produces more accurate control of the attack-angle, sideslip angle and the rate of the bank angle about the velocity vector, and smaller control deflections compared with the dynamic-inversion controller.
作者 朱秋芳 姜长生 朱亮 谢祥华
机构地区 南京航空航天大学自动化学院
出处 《南京航空航天大学学报》 EI CAS CSCD 北大核心 2007年第3期379-383,共5页 Journal of Nanjing University of Aeronautics & Astronautics
基金 国家自然科学基金项目(90405011)资助项目
关键词 轨迹线性化控制(TLC) 超机动 飞行控制系统 仿真 trajectory linearization control super-maneuverable flight control system simulation
分类号 V294.1 [航空宇航科学技术]
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参考文献7

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同被引文献43

  • 1陈谋,姜长生,吴庆宪.基于多模型方法的全包络鲁棒飞行控制器设计[J].航空学报,2006,27(3):486-492. 被引量：15
  • 2朱亮,姜长生,方炜.基于非线性干扰观测器的不确定非线性系统鲁棒轨迹线性化控制[J].信息与控制,2006,35(6):705-710. 被引量：8
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引证文献6

二级引证文献15

南京航空航天大学学报
2007年 第3期

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