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反馈线性化及其在飞控系统中的应用 被引量:1

Feedback Linearization and Its Application to Flight Control Systems
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摘要 反馈线性化方法是一种有效的解决非线性系统控制的方法[1] 。而未来新一代战机控制系统需要适应超机动作战的非线性控制 ,非线性控制系统是必然要采用的。文中先简要介绍了反馈线性化理论 ,然后介绍了反馈线性化方法在飞控系统中的具体应用 ,最后以某型号先进战斗机为仿真算例进行了仿真 ,仿真结果表明 ,基于反馈线性化方法设计的飞控系统是可行的。 Feedback linearization is a effective approach to a nonlinear control system. A major feature of next generation fighter aircraft is supermaneuver ability, and its control system must be a nonlinear control system. First, a feedback linearization theory is presented briefly, then the application of feedback linearization to flight controls is described. Finally simulation about anadvanced fighter aircraft are presented. According to the result of simulation,a conclusion can be made that the application to flight control systems is feasible and effective.
出处 《飞机设计》 2004年第2期42-46,共5页 Aircraft Design
关键词 反馈线性化 仿真结果 非线性系统 新一代 非线性控制系统 算例 型号 超机动 战斗机 战机 feedback linearization nonlinear flight control system
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参考文献2

  • 1[3]Bugajski D J,Enns D F.Nonlinear Control Law with Application to High Angle-of-Attack Flight.Journal of Guidance ,ontrol,nd Dynamics,1992,15(3):761-767.
  • 2[4]Snell S A, Enns D F.Nonlinear Inversion Flight Control for a Supermaneuverable Aircraft.Journal of Guidance ,ontrol,and Dynamics,1992,15(4):976-984.

同被引文献5

  • 1高彦玺,王衍洋,金长江.推力矢量控制与飞机过失速机动仿真研究[J].飞行力学,1997,15(1):23-29. 被引量:11
  • 2[1]Bugajski D J,Enns D f.Nonlinear control law with application to high angle-of-attack flight[J].Journal of Guidance Control and Dynamics,1992,15(3):761-767.
  • 3[3]Sepulchre R,Jankovic M,Vokotovic P V.Interlaced systems and recursive designs for global stabilization[C].Proceedings of the 1997 European Control Conference,1997.
  • 4[4]Harkegard O,Glad S T.A backstepping design for flight path angle control[C].Proceedings of 39 th Conference on Decision and Control,2000.
  • 5[5]Lee T Y,Kim Y D.Nonlinear adaptive flight control using backstepping and neural networks controller[J].Journal of Guidance Control and Dynamics,2001,24(4):675-682.

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