Design of robust gain scheduled hold control system

Design of robust gain scheduled hold control system

О. I. Nadsadna



This paper represents an strategy to tune robust control system on the example of pitch holdmode for small unmanned aerial vehicles by using gain scheduling proportional-integral-derivative controlalgorithms. The simulation of controlled flight dynamics modeling with changing flight conditions andtaking into account the action of stochastic disturbances prove the efficiency of the proposed procedure.This technique is useful to obtain flexibility and robustness in the controller’s automatic design


gain scheduling; PID controller; robustness; penalty function; unmanned aerial vehicle


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