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双旋翼直升机系统建模与鲁棒控制器设计

摘要第4-5页
Abstract第5页
Chapter 1 Introduction第8-15页
    1.1 Background第8-10页
    1.2 Significance of the Study第10页
    1.3 Problem Statement第10-11页
        1.3.1 Main Objective第11页
        1.3.2 Specific Objectives第11页
    1.4 Literature Review第11-15页
Chapter 2:System Modeling第15-33页
    2.1 Introduction第15-20页
    2.2 Linearization of the Dyamic Equation第20页
    2.3 State Feedback Controller Design第20-24页
    2.4 Uncertain System Modeling第24-33页
Chapter 3:Controller Design第33-68页
    3.1 Introduction第33-34页
    3.2 The H_∞Optimization Approach第34-46页
        3.2.1 Robust Analysis of the H_∞Optimal Controller第41-46页
    3.3 H_∞Loop Shaping Procedure Controller Design第46-53页
        3.3.1 Loop Shaping design procedure第46-49页
        3.3.2 Robust Analysis of the LSDP Controller第49-53页
    3.4 μ-Synthesis and D-K iterations method第53-63页
        3.4.1 Robust Stability and Performance of第57-63页
    3.5 Comparison of the H_∞LSDP and μ-controllers第63-64页
        3.5.1 Frequency responses of the controller第63页
        3.5.2 Response of the nominal closed loop systems with the controllers第63-64页
    3.6 Robust stability comparison of the three controllers第64-68页
Chapter 4 : Uncertain System modeling for the TRHS Linearized at π/2第68-79页
    4.1 Desin of the H_∞ suboptimal controller第72-73页
    4.2 Results and Analysis of the Closed Loop System with the Sub-optimalcontroller第73-78页
    4.3 Simulations Results and Experiments第78-79页
Conclusion第79-81页
结论第81-84页
References第84-89页
Acknowledgement第89页

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