Usually the missile attitude control process in a large flight envelope has strong time-varying and nonlinear characteristics, so the controller parameter is difficultly scheduled with conventional PID control approach. In this study a linear active disturbance rejection control approach based on reduced-order linear extended state observer is proposed. The approach is employed to the attitude controller for a supersonic missile in attack with high angle. It is not hard to determine the proposed controller parameter, and the numeral simulations show that the presented approach has a very good capability on tracking attitude command.
Missile attitude control in a large flight envelope based on the linear active disturbance rejection control approach
2014-08-01
123717 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Research on Aircraft Attitude Control Method Based on Linear Active Disturbance Rejection
DOAJ | 2022
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