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Parameter design for a guidance and control system using genetic approach

机译:基于遗传方法的制导系统参数设计

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摘要

A preliminary guidance and control design for guided missiles is developed via a genetic searching approach. A real-coded genetic algorithm (RGA) serves as the computing device to solve a constrained optimization problem resulting form the guidance and control parameter deign where the genetic structure encodes some sort of automation. It is a global search algorithm thus avoids a local minimum. This new design paradigm offers a way to implement simple but robust solutions that cover a wide range of aerodynamic variations. Simulation results are performed to illustrate the enegagement performance and applicability of this proposed design.
机译:通过遗传搜索方法开发了制导导弹的初步制导和控制设计。实编码遗传算法(RGA)用作计算设备,用于解决由指导和控制参数确定而导致的约束优化问题,其中遗传结构对某种自动化进行编码。它是一种全局搜索算法,因此避免了局部最小值。这种新的设计范例提供了一种实现简单而强大的解决方案的方法,该解决方案涵盖了广泛的空气动力学变化。仿真结果表明了该拟议设计的啮合性能和适用性。

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