Unmanned aerial vehicle (UAV) was designed to fulfill its mission autonomously. Its core technology for successful development of the UAV is to design of the flight control system (FCS) consisting of the flight control computer, the actuator, the sensor in order to replace the pilot. Each development procedure of FCS involves a verifying test for each step and was completed by an evaluation test of the comprehensive performance verification for the overall systems. The development tool, which is applied to this objective, is the HILS (Hardware-In-the-Loop-Simulation). That is, HILS is a cost-effective method for testing complex, flight-critical hardware before it is used in the real world. The real-time HILS is shown to develop/verify the performance of SURV UAV's controller in the lateral/directional control systems.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    The verification of UAV's autopilot system with realtime HILS


    Contributors:

    Conference:

    ICMIT 2005: Control Systems and Robotics ; 2005 ; Chongqing,China


    Published in:

    Publication date :

    2005-12-22





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    The Design Tools for UAV's Autopilot Solution

    Kanovsky, P. / Nohyl, J. / Smrcek, L. et al. | British Library Conference Proceedings | 2004


    Design of autopilot platform using HILS approach

    Elsadig, Mohammed A. / Elbakri, Mohamed A. | IEEE | 2017


    HILS DRONE HILS SYSTEM FOR DETECTING EXPLOSIVES

    YANG JUN HO / SUK JIN YOUNG / PARK JEONG SIK et al. | European Patent Office | 2023

    Free access

    HILS HILS-based ship maneuverability measurement and management system

    JANG PIL SOON / GANG YONG SOO | European Patent Office | 2018

    Free access

    HILS BRAKE HILS SYSTEM FOR A RAILWAY VEHICLE

    European Patent Office | 2019

    Free access