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The tactical missile autopilot design process is detailed from a backstepping control perspective. Wherein, two autopilot topologies are proposed, i.e. the angle of attack (AOA) autopilot and acceleration autopilot. The nonlinear missile longitudinal dynamics is dealt with firstly to meet the strict feedback form. Control parameters of AOA autopilot are introduced in turn and required to be positive...
A new PID parameter self-tuning algorithm is proposed, which adapts to single plant. Guaranteeing the stabilization of closed loop systems and satisfying the conditions of self-tuning, we can use recursion least squares method and estimate the change of model parameter of the plant online. The PID self-tuning control algorithm is applied to control and research the real-time temperature of the resistance...
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