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A nonsingular terminal guidance law is proposed for dual-controlled missile with tails and reaction jets based on power rate reaching law and neural network terminal sliding mode control (TSMC). By combining nonsingular terminal sliding mode control (NTSMC) with power rate reaching law, the guidance law improves the reaching rate of system states to sliding surface with less control command. Also,...
For flight control systems with time-varying delay, an H ∞ output tracking controller is proposed. The controller is designed for the discrete-time state-space model of general aircraft to reduce the effects of uncertainties of the mathematical model, external disturbances, and bounded time-varying delay. It is assumed that the feedback-control loop is closed by the communication network,...
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