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.
Retuning the actuator proportional–integral–derivative controller of spinning missiles
2017
Aufsatz (Zeitschrift)
Englisch
Retuning the actuator proportional–integral–derivative controller of spinning missiles
SAGE Publications | 2017
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