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提出基于反馈线性化理论的BTT导弹自动驾驶仪设计方法。并提出由俯仰过载命令产生攻角命令的方法。应用CMAC神经网络构成一种自适应反馈线性化方案,使具有不确定性的实际系统获得要求的跟踪性能。闭环系统的稳定性由李雅普诺夫稳定性理论得到保证。该方法适合于控制导弹作全空域飞行。
A design method of BTT missile autopilots based on feedback linearization theory is proposed. And proposes a method of generating an angle-of-attack command by a pitch over-load command. The application of CMAC neural network to form an adaptive feedback linearization scheme can make the actual system with the uncertainty get the required tracking performance. The stability of the closed-loop system is guaranteed by Lyapunov stability theory. The method is suitable for controlling missiles for full airspace flight.