Act of nonlinear proportional derivative controller for MFC laminated shell

2020 ◽  
Vol 95 (9) ◽  
pp. 095210
Author(s):  
H S Bauomy ◽  
A T EL-Sayed
Author(s):  
Wei Zhou ◽  
Shuxing Yang ◽  
Liangyu Zhao

The hinge moment acting on the actuator will cause an out-of-plane moment, which is a destabilizing factor to the angular motion of spinning missiles. A new tuning criterion for the actuator controller is proposed to decrease the out-of-plane moment. It is noted that the integral element does not decrease the out-of-plane moment. A carefully designed proportional–derivative controller with some compromises can ensure the stability of the missile and provide good performance for the actuator.


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