• DocumentCode
    2902154
  • Title

    Modular scalable system for operation and testing of UAVs

  • Author

    Laiacker, M. ; Klockner, Andreas ; Kondak, K. ; Schwarzbach, M. ; Looye, Gertjan ; Sommer, D. ; Kossyk, Ingo

  • Author_Institution
    Robot. & Mechatron. Center, German Aerosp. Center (DLR), Wessling, Germany
  • fYear
    2013
  • fDate
    17-19 June 2013
  • Firstpage
    1460
  • Lastpage
    1465
  • Abstract
    In this paper we present a system for operation and testing of different UAVs. The system allows easy development and modification of control and mission software. The system is composed of hard- and software modules with a standardized interface. We have been using the system with rotary and fixed wing UAVs with a take-off mass between 10 and 100 kg. For larger platforms the system can be used in a redundant setup. The software modules are integrated in a special real-time framework, which supports execution, scheduling, communication and system monitoring. A modular simulation and control infrastructure allows for flexible, integrated design and analysis of control laws. The code for the computational part of the modules can be generated from Matlab/Simulink-models or from Modelica-models. The system supports debugging, soft- and hardware in the loop simulations, operator training as well as real flight experiments. The main design concepts are explained at hand of our solar powered high altitude platform ELHASPA and the 10 years experience in development and operation will be summarized.
  • Keywords
    aerospace components; aerospace computing; autonomous aerial vehicles; computer debugging; control engineering computing; mechanical engineering computing; mobile robots; vehicle dynamics; ELHASPA; Matlab-Simulink-models; Modelica-models. The; communication monitoring; control law integrated analysis; control law integrated design; control software modification; debugging; execution monitoring; fixed wing UAV; hardware-in-the-loop simulations; mass 10 kg; mass 100 kg; mission software modification; modular scalable system; rotary wing UAV; scheduling monitoring; software-in-the-loop-simulations; solar powered high altitude platform; system monitoring; take-off mass; Actuators; Adaptation models; Atmospheric modeling; Hardware; Mathematical model; Software; Solid modeling;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference (ACC), 2013
  • Conference_Location
    Washington, DC
  • ISSN
    0743-1619
  • Print_ISBN
    978-1-4799-0177-7
  • Type

    conf

  • DOI
    10.1109/ACC.2013.6580042
  • Filename
    6580042