Helicopter being highly coupled and complex nonlinear system is difficult not only from modeling perspective but also from control design. Hence, it must be ensured that designed control system will make helicopter flight safe and will improve efficiency of completing mission. This work aim is to present different control techniques for attitude control of helicopter. The attitude is implemented using Matlab/Simulink. The different control techniques implemented for attitude dynamics of helicopter are mixed sensitivity design and Increment-Proportional-Integral-Derivative (IPID) controller. These control techniques performance is individually studied for attitude model. It is observed that the performance of these controllers is very effective and significant. The improvement in the performance of attitude control system can be judged from the simulation results obtained. These control techniques can be implemented for flight control system design.


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    Title :

    Helicopter attitude control


    Contributors:


    Publication date :

    2018-03-01


    Size :

    525068 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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