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- W2376677897 abstract "A very severe nonlinear is presented because flight parameters vary along with the flight condition in the flight of the homing gliding missile which brings much difficulty to the design of control system.A new design method using fuzzy-PID control combined the advantages of fuzzy control and PID control is presented,and thoughts are proposed for the homing gliding missile autopilot design.This approach can partly avoid the blindness of the PID parameters' acquirement which is usually gained by chance in the design of autopilots.The results of simulation show that the design method is able to provide a better relative stability and robustness." @default.
- W2376677897 created "2016-06-24" @default.
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- W2376677897 date "2005-01-01" @default.
- W2376677897 modified "2023-09-23" @default.
- W2376677897 title "Application of the Fuzzy-PID Control to the Roll Stabilized Loop of the Homing Gliding Missile" @default.
- W2376677897 hasPublicationYear "2005" @default.
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