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数据链指挥下的战斗机H_∞飞行控制器设计 被引量:5

Design of H_∞ Flight Controller for Fighter under Tactical Data-link Command
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摘要 基于神经网络对数据链指挥下的战斗机提出了鲁棒飞行控制器设计方案.为了克服由于数据链的引入对战斗机飞行控制所带来的不利影响,设计了基于RBF神经网络的鲁棒飞行控制器.通过对神经网络参数在线调整,使飞行控制系统能跟踪期望指令,并满足给定的性能指标.最后将所设计的飞行控制系统用于数据链指挥下的战斗机飞行控制,仿真结果表明所设计的飞行控制系统是有效的. t An H∞ flight control scheme is proposed based on neural network for the fighter under the command of tactical data-link. For overcoming the influence due to introducing the tactical data-link, the H∞ flight control scheme is presented for the fighter. The online adjusted parameters are introduced to make flight controller system track the expected command signal and satisfy the given performance index. Finally, the availability of the designed robust flight control system is demonstrated through a flight simulation, and the simulation results suggest the H∞ flight control scheme is valid.
出处 《自动化学报》 EI CSCD 北大核心 2008年第2期211-214,共4页 Acta Automatica Sinica
基金 国家自然科学基金(90405011 90716028)资助~~
关键词 时延非线性系统 飞行控制 鲁棒控制 H∞控制 Time delay nonlinear system, flight control, robust control, H∞ control
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参考文献3

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同被引文献43

  • 1李正强,张怡哲,宋述杰,邓建华.非线性结构自适应模型逆飞行控制律设计研究[J].西北工业大学学报,2009,27(4):471-476. 被引量:2
  • 2朱铁夫,李明,邓建华.存在多输入未建模动态的鲁棒控制[J].西北工业大学学报,2004,22(4):435-438. 被引量:4
  • 3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
  • 4朱秋芳,姜长生,朱亮,谢祥华.采用TLC方法的超机动飞行控制系统设计[J].南京航空航天大学学报,2007,39(3):379-383. 被引量:6
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