This paper describes the design methodology of Hardware In Loop Simulation (HILS) for advanced aerospace vehicle. It exploits detailed six degree of freedom (6DOF) model for an asymmetrically configured aerospace vehicle. Criticalities exist in modelling and simulation of the vehicle has been discussed in detail. It explains the nonlinearities present in the actuators of the vehicle and its effect on the vehicle dynamics. Initially simulation is performed by integrating all subsystem models in a single Non Real Time (NRT) simulation test setup. Further HILS is carried out by replacing model with actual hardware in a stepwise manner. Simulation results of the vehicle are presented and also comparative results on actuator nonlinearities are presented.


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    Titel :

    Hardware In Loop Simulation of Advanced Aerospace Vehicle


    Weitere Titelangaben:

    Learning and Analytics in Intelligent Systems


    Beteiligte:
    Satapathy, Suresh Chandra (Herausgeber:in) / Raju, K. Srujan (Herausgeber:in) / Shyamala, K. (Herausgeber:in) / Krishna, D. Rama (Herausgeber:in) / Favorskaya, Margarita N. (Herausgeber:in) / Shiva Krishna Prasad, A. (Autor:in) / Susheela, N. (Autor:in)

    Kongress:

    International Conference on E-Business and Telecommunications ; 2019 ; Hyderabad, India March 22, 2019 - March 23, 2019



    Erscheinungsdatum :

    26.07.2019


    Format / Umfang :

    9 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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