Neural network based control system design of an advanced fighter aircraft

A. Bhatti
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引用次数: 1

Abstract

The author demonstrates the application of neural network technology to optimal scheduling of control gains in real-time flight control systems commonly used in the real-time control of an advanced fighter aircraft and high-performance aerospace vehicles where a priori target outputs are not known, and must be generated in real-time. A learning algorithm and an appropriate performance model have been used to synthesize a nonlinear functional relationship between varying plant parameters and control gains. A performance model is used to exemplify the desired responses and force the plant/controller dynamics via a neural network to imitate the model. The performance model contains the proper dynamics to supply desired responses to given test inputs. An arbitrary cost function is used to indicate the quality of plant/controller performance according to which the adjustments to the weights within the neural network are made by the learning algorithm. The process is repeated until the neural network produces an optimal set of gains for each point in the plant parameter space.<>
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基于神经网络的先进战斗机控制系统设计
作者演示了神经网络技术在实时飞行控制系统中控制增益最优调度的应用,该系统通常用于先进战斗机和高性能航天飞行器的实时控制,其先验目标输出是未知的,必须实时生成。采用一种学习算法和适当的性能模型来综合变化的对象参数与控制增益之间的非线性函数关系。性能模型用于举例说明期望的响应,并通过神经网络强制植物/控制器动态模仿该模型。性能模型包含适当的动态,为给定的测试输入提供所需的响应。使用任意的代价函数来指示设备/控制器性能的质量,学习算法根据该函数对神经网络内的权重进行调整。这个过程不断重复,直到神经网络为植物参数空间中的每个点产生一组最优增益
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