基于神经网络动态逆的巡逻导弹自动驾驶仪设计
Dynamic Inversion Autopilot Design for Loiter Missile Based on Neural Network
Received date: 2010-03-24
Online published: 2025-05-28
杜大程 , 刘莉 , 李怀建 , 于剑桥 . 基于神经网络动态逆的巡逻导弹自动驾驶仪设计[J]. 弹箭与制导学报, 2010 , 30(6) : 42 -45 . DOI: 10.15892/j.cnki.djzdxb.2010.06.036
A nonlinear dynamic inversion control method based on neural network is applied for loiter missile autopilot design. Firstly, the dynamics of the missile are separated into a fast part and a slow part based on the two time-scale assumption. Then dynamic inversion control method is appliyed for both the two parts. The neural networks(NN) are adopted to compensate the dynamic inversion error casued by inaccuracy of model and system parameter perturbation. The adjustment arithmetic of NN weight is given and stability of the closed loop system is proved. Finally, the simulation results demonstrate that the method proposed overcomes the shortage of nonlinear dynamical inversion control scheme where a precise mathematic model is necessary and system robustness has improved. The effectiveness of the nonlinear control scheme is proved.
Key words: autopilot; dynamic inversion; neural networks; nonlinear control
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