In order to achieve maximum noise reduction inside an aircraft cabin through the use of an active noise control system (ANCS), it is important that the number and positions of the sensors for monitoring the noise field; the control system for driving the actuators; and the number and positions of the actuators that generate the secondary noise field, which partially cancels the primary noise field, must be optimally determined. An optimization strategy for the positioning of the actuators, based on genetic algorithms (GA), is presented, assuming a fixed sensor configuration and a given control system. The application of the developed GA to a propeller aircraft is also discussed. The work presented was performed under the CEC BRITE/EURAM-Aeronautics project “ASANCA”, in which a demonstrator ANCS was developed.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    A genetic algorithm for optimal positioning of actuators in active noise control: results from the ASANCA project


    Contributors:

    Published in:

    Publication date :

    2000-06-01


    Size :

    7 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





    Selected Flight Test Data and Control System Results of the ASANCA Project

    Borchers, I. U. et al. / Commission of the European Communities | British Library Conference Proceedings | 1993



    Optimal Placement of Actuators for Active Vibration Control Using EER and Genetic Algorithm

    Chen, Jianding / Jiang, Jinhui / Wang, Ke et al. | IEEE | 2019