Titlebook: Linear and Nonlinear Control of Small-Scale Unmanned Helicopters; Ioannis A. Raptis,Kimon P. Valavanis Book 2011 Springer Science+Business

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Intelligent Systems, Control and Automation: Science and Engineeringhttp://image.papertrans.cn/l/image/586463.jpg

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Simplified Rotor Dynamics,n characteristics and controls. Due to the complexity and the uncertainty associated with the aerodynamic phenomena, a detailed model of the forces and moments produced by the main rotor would be of high order and completely impractical for any controller design. In this Chapter, the modeling approa

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Frequency Domain System Identification,his mathematical model is represented by a set of ordinary differential equations. Establishing such a model for helicopters is a challenging task. This Chapter provides a thorough description of a frequency domain identification procedure for the extraction of linear models that correspond to certa

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Time Domain Parameter Estimation and Applied Discrete Nonlinear Control for Small-Scale Unmanned Hel identification and control solution for direct application to an autonomous helicopter flight system. Although most controller designs are in continuous time, this Chapter considers the discrete time dynamics of the helicopter. The shift of the helicopter control problem to discrete time is twofol

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