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Eigenstructure Assignment Based Flight Control for Advanced Fighter: An Optimization Based Approach

机译:基于特征结构分配的高级战斗机飞行控制:一种基于优化的方法

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An intelligent optimization approach is proposed for eigenstructure assignment (EA) via neural network (NN) adjusting the components of output vector autonomously. The Basic idea is to minimize the L2 norm of error between the desired vector and achievable vector using the designing freedom provided by EA technique. Besides, close-loop eigenvalues are also optimised within desired regions on the left-half complex plane according to the design objective to ensure both closed-loop stability and dynamical performance. With the proposed approach, additional closed-loop specifications such as decoupling of different modes and robustness can also be easily achieved. As a demonstration, application of the proposed approach to the designing of flight control law for an advanced fighter is discussed. The simulation results show good closed loop performance and validate the proposed intelligent optimization approach of EA technique.
机译:提出了一种通过神经网络(NN)自动调整输出矢量分量的特征结构分配(EA)的智能优化方法。基本思想是使用EA技术提供的设计自由度,将所需矢量和可实现矢量之间的L2范数最小化。此外,还根据设计目标在左半复杂平面上的期望区域内优化了闭环特征值,以确保闭环稳定性和动态性能。使用所提出的方法,还可以轻松实现其他闭环规范,例如不同模式的解耦和鲁棒性。作为演示,讨论了所建议的方法在高级战斗机的飞行控制法设计中的应用。仿真结果显示了良好的闭环性能,并验证了所提出的EA技术的智能优化方法。

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