Design of Aircraft Cockpit Cover Heating System Based on Cascade PID

Design of Aircraft Cockpit Cover Heating System Based on Cascade PID

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The cockpit cover heating loading test-bed is one of the most effective ways to verify whether the aerodynamic heating and aerodynamic loading will lead to the fatigue failure of the cockpit cover, however, in the process of Beta Sitosterol designing and building the test-bed, it is inevitable to encounter the problems such as the lag and overshoot of the surface temperature field of the canopy.Under the background of heating the cabin cover by AC heat exchange, the heating system is modeled, and the design schemes of cascade PID (Proportion Integration Differentiation) regulator and heating control system are given respectively, and the control effect is analyzed.The results show that the heating control system designed in this paper can effectively solve the problem of temperature field lag Heat Emitters and overshoot in the heating process, and is of high sensitivity.