Adaptive fuzzy mixed H2 / H lateral control of nonlinear missile systems

Yung-Yu Chen, Bor Sen Chen, Chung Shi Tseng

研究成果: Paper

摘要

An adaptive fuzzy mixed H2 / H lateral control of nonlinear missile systems with uncertain disturbances considered is proposed to achieve H2 quadratic tracking with Hdisturbance rejection. This approach can be applied to control the lateral directional dynamics of the missiles at high angle of attack or generate moments on missile operating in flight regimes where the effectiveness of conventional aerodynamic surfaces is reduced. Using an adaptive fuzzy approximation method, the uncertain nonlinear model of the missile system is estimated. Then, by a mixed H2 / H control design, the effects of external disturbance and fuzzy approximation error as well as consumed energy of the controller is minimized. By the skew symmetric property of the missile system and adequate choice of state variable transformation, this problem can be reduced to solve two algebraic Riccati-like equations. Furthermore, a closed-form solution to these two algebraic equations can be obtained with very simple form for the preceding control design. This work was supported by National Science Council, Taiwan, R.O . C., under grant NSC 91-2213-E-007-014.

原文English
頁面512-516
頁數5
出版狀態Published - 2003 七月 11
事件The IEEE International conference on Fuzzy Systems - St. Louis, MO, United States
持續時間: 2003 五月 252003 五月 28

Other

OtherThe IEEE International conference on Fuzzy Systems
國家United States
城市St. Louis, MO
期間03-05-2503-05-28

指紋

Missile
Missiles
Lateral
Control Design
Disturbance
Variable Transformation
Taiwan
Approximation Error
Angle of attack
Rejection
Closed-form Solution
Approximation Methods
Algebraic Equation
Aerodynamics
Skew
Nonlinear Model
Attack
Moment
Controller
Angle

All Science Journal Classification (ASJC) codes

  • Software
  • Theoretical Computer Science
  • Artificial Intelligence
  • Applied Mathematics

引用此文

Chen, Y-Y., Chen, B. S., & Tseng, C. S. (2003). Adaptive fuzzy mixed H2 / H lateral control of nonlinear missile systems. 512-516. 論文發表於 The IEEE International conference on Fuzzy Systems, St. Louis, MO, United States.
Chen, Yung-Yu ; Chen, Bor Sen ; Tseng, Chung Shi. / Adaptive fuzzy mixed H2 / H lateral control of nonlinear missile systems. 論文發表於 The IEEE International conference on Fuzzy Systems, St. Louis, MO, United States.5 p.
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Chen, Y-Y, Chen, BS & Tseng, CS 2003, 'Adaptive fuzzy mixed H2 / H lateral control of nonlinear missile systems' 論文發表於 The IEEE International conference on Fuzzy Systems, St. Louis, MO, United States, 03-05-25 - 03-05-28, 頁 512-516.

Adaptive fuzzy mixed H2 / H lateral control of nonlinear missile systems. / Chen, Yung-Yu; Chen, Bor Sen; Tseng, Chung Shi.

2003. 512-516 論文發表於 The IEEE International conference on Fuzzy Systems, St. Louis, MO, United States.

研究成果: Paper

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N2 - An adaptive fuzzy mixed H2 / H∞ lateral control of nonlinear missile systems with uncertain disturbances considered is proposed to achieve H2 quadratic tracking with H∞disturbance rejection. This approach can be applied to control the lateral directional dynamics of the missiles at high angle of attack or generate moments on missile operating in flight regimes where the effectiveness of conventional aerodynamic surfaces is reduced. Using an adaptive fuzzy approximation method, the uncertain nonlinear model of the missile system is estimated. Then, by a mixed H2 / H∞ control design, the effects of external disturbance and fuzzy approximation error as well as consumed energy of the controller is minimized. By the skew symmetric property of the missile system and adequate choice of state variable transformation, this problem can be reduced to solve two algebraic Riccati-like equations. Furthermore, a closed-form solution to these two algebraic equations can be obtained with very simple form for the preceding control design. This work was supported by National Science Council, Taiwan, R.O . C., under grant NSC 91-2213-E-007-014.

AB - An adaptive fuzzy mixed H2 / H∞ lateral control of nonlinear missile systems with uncertain disturbances considered is proposed to achieve H2 quadratic tracking with H∞disturbance rejection. This approach can be applied to control the lateral directional dynamics of the missiles at high angle of attack or generate moments on missile operating in flight regimes where the effectiveness of conventional aerodynamic surfaces is reduced. Using an adaptive fuzzy approximation method, the uncertain nonlinear model of the missile system is estimated. Then, by a mixed H2 / H∞ control design, the effects of external disturbance and fuzzy approximation error as well as consumed energy of the controller is minimized. By the skew symmetric property of the missile system and adequate choice of state variable transformation, this problem can be reduced to solve two algebraic Riccati-like equations. Furthermore, a closed-form solution to these two algebraic equations can be obtained with very simple form for the preceding control design. This work was supported by National Science Council, Taiwan, R.O . C., under grant NSC 91-2213-E-007-014.

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Chen Y-Y, Chen BS, Tseng CS. Adaptive fuzzy mixed H2 / H lateral control of nonlinear missile systems. 2003. 論文發表於 The IEEE International conference on Fuzzy Systems, St. Louis, MO, United States.