Adaptive block dynamic surface control for integrated missile guidance and autopilot
A novel integrated guidance and autopilot design method is proposed for homing missiles based on the adaptive block dynamic surface control approach. The fully integrated guidance and autopilot model is established by combining the nonlinear missile dynamics with the nonlinear dynamics describing th...
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| Published in | Chinese journal of aeronautics Vol. 26; no. 3; pp. 741 - 750 |
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| Main Authors | , , |
| Format | Journal Article |
| Language | English |
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Elsevier Ltd
01.06.2013
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| Online Access | Get full text |
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| Abstract | A novel integrated guidance and autopilot design method is proposed for homing missiles based on the adaptive block dynamic surface control approach. The fully integrated guidance and autopilot model is established by combining the nonlinear missile dynamics with the nonlinear dynamics describing the pursuit situation of a missile and a target in the three-dimensional space. The integrated guidance and autopilot design problem is further converted to a state regulation problem of a time-varying nonlinear system with matched and unmatched uncertainties. A new and simple adaptive block dynamic surface control algorithm is proposed to address such a state regulation problem. The stability of the closed-loop system is proven based on the Lyapunov theory. The six degrees of freedom （6DOF） nonlinear numerical simulation results show that the proposed integrated guidance and autopilot algorithm can ensure the accuracy of target interception and the robust stability of the closed-loop system with respect to the uncertainties in the missile dynamics. |
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| AbstractList | A novel integrated guidance and autopilot design method is proposed for homing missiles based on the adaptive block dynamic surface control approach. The fully integrated guidance and autopilot model is established by combining the nonlinear missile dynamics with the nonlinear dynamics describing the pursuit situation of a missile and a target in the three-dimensional space. The integrated guidance and autopilot design problem is further converted to a state regulation problem of a time-varying nonlinear system with matched and unmatched uncertainties. A new and simple adaptive block dynamic surface control algorithm is proposed to address such a state regulation problem. The stability of the closed-loop system is proven based on the Lyapunov theory. The six degrees of freedom (6DOF) nonlinear numerical simulation results show that the proposed integrated guidance and autopilot algorithm can ensure the accuracy of target interception and the robust stability of the closed-loop system with respect to the uncertainties in the missile dynamics. A novel integrated guidance and autopilot design method is proposed for homing missiles based on the adaptive block dynamic surface control approach. The fully integrated guidance and autopilot model is established by combining the nonlinear missile dynamics with the nonlinear dynamics describing the pursuit situation of a missile and a target in the three-dimensional space. The integrated guidance and autopilot design problem is further converted to a state regulation problem of a time-varying nonlinear system with matched and unmatched uncertainties. A new and simple adaptive block dynamic surface control algorithm is proposed to address such a state regulation problem. The stability of the closed-loop system is proven based on the Lyapunov theory. The six degrees of freedom （6DOF） nonlinear numerical simulation results show that the proposed integrated guidance and autopilot algorithm can ensure the accuracy of target interception and the robust stability of the closed-loop system with respect to the uncertainties in the missile dynamics. |
| Author | Hou Mingzhe Liang Xiaoling Duan Guangren |
| AuthorAffiliation | Center for Control Theory and Guidance Technology, Harbin Institute of Technology, Harbin 150001, China |
| Author_xml | – sequence: 1 givenname: Mingzhe surname: Hou fullname: Hou, Mingzhe email: hithyt@gmail.com – sequence: 2 givenname: Xiaoling surname: Liang fullname: Liang, Xiaoling email: lxl_dmu2008@126.com – sequence: 3 givenname: Guangren surname: Duan fullname: Duan, Guangren email: g.r.duan@hit.edu.cn |
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| Cites_doi | 10.1109/TCST.2006.876903 10.1007/s12555-011-0121-7 10.2514/1.34291 10.2514/1.36961 10.1109/7.543873 10.1016/S0967-0661(01)00082-X 10.2514/1.24953 10.2514/6.1999-4078 10.1007/s11633-010-0563-z 10.1080/002071798221650 10.2514/6.2004-4880 10.1016/S1000-9361(08)60021-7 10.1109/TAC.2000.880994 10.1109/ICMA.2009.5244807 |
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| Keywords | Integrated guidance and autopilot Block dynamic surface control Adaptive control Missile control Nonlinear control |
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| Notes | Adaptive control; Block dynamic surface control; Integrated guidance and autopilot; Missile control; Nonlinear control A novel integrated guidance and autopilot design method is proposed for homing missiles based on the adaptive block dynamic surface control approach. The fully integrated guidance and autopilot model is established by combining the nonlinear missile dynamics with the nonlinear dynamics describing the pursuit situation of a missile and a target in the three-dimensional space. The integrated guidance and autopilot design problem is further converted to a state regulation problem of a time-varying nonlinear system with matched and unmatched uncertainties. A new and simple adaptive block dynamic surface control algorithm is proposed to address such a state regulation problem. The stability of the closed-loop system is proven based on the Lyapunov theory. The six degrees of freedom （6DOF） nonlinear numerical simulation results show that the proposed integrated guidance and autopilot algorithm can ensure the accuracy of target interception and the robust stability of the closed-loop system with respect to the uncertainties in the missile dynamics. 11-1732/V ObjectType-Article-1 SourceType-Scholarly Journals-1 ObjectType-Feature-2 content type line 23 |
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| SubjectTerms | Adaptive control Adaptive control systems Automatic pilots Block dynamic surface control Blocking Design engineering Dynamical systems Integrated guidance and autopilot Lyapunov稳定性理论 Mathematical models Missile control Missiles Nonlinear control Nonlinear dynamics Nonlinearity 全集成 导弹制导 控制算法 时变非线性系统 自动驾驶仪 自适应 非线性动力学 |
| Title | Adaptive block dynamic surface control for integrated missile guidance and autopilot |
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