A continuation design framework for nonlinear flight control problems

T. S. Richardson; M. H. Lowenberg

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A continuation design framework for nonlinear flight control problems

机译：非线性飞行控制问题的连续设计框架

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A methodology referred to as the continuation design framework is developed for application to nonlinear flight control problems. This forms the basis of a systematic approach to control system design for aircraft operating in highly nonlinear regions of the flight envelope. The essence of the continuation design framework is to combine bifurcation analysis with modern control methods such as eigenstructure assignment. Theoretical and practical issues of the approach are discussed with particular reference to the problems posed by agile fighter aircraft. The proposed methodology is applied to a fifth order hypothetical aircraft model and is shown to provide a visible, flexible and logical approach to nonlinear aircraft control law design.

机译：开发了一种称为连续性设计框架的方法，用于非线性飞行控制问题。这形成了在飞行包络线的高度非线性区域中运行的飞机的控制系统设计的系统方法的基础。延续设计框架的实质是将分叉分析与现代控制方法（例如本征结构分配）结合起来。讨论了该方法的理论和实践问题，并特别参考了敏捷战斗机带来的问题。所提出的方法应用于五阶假设飞机模型，并被证明为非线性飞机控制律设计提供了一种可见，灵活和逻辑的方法。

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来源
《The Aeronautical Journal》 |2006年第1104期|p.85-96|共12页
作者
T. S. Richardson; M. H. Lowenberg;
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作者单位

Department of Aerospace Engineering University of Bristol, UK;

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正文语种 eng
中图分类航空;
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A continuation design framework for nonlinear flight control problems

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