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access icon openaccess Rapid-prototyping and hardware-in-the-loop laboratory platform for development and testing of electro-mechanical actuator controls

To meet the challenges posed by the increasing use of electrical actuation on board next generation aircraft, advanced experimental testing capabilities are required to investigate optimal system design, performance and control. Rapid control-prototyping and hardware-in-the-loop (HiL) techniques provide the ability to expedite experimental testing, allowing for elements of the system to be validated without requiring fully realised hardware. Previously, this would require large scale laboratory setups, where the entire electrical and mechanical system would have to be designed and built prior to experimental testing. This study presents the development of a laboratory HiL and rapid-prototyping test-bench, capable of investigating the performance of actuator motor control schemes, under a variety of test conditions. Experimental testing is carried out using a laboratory test-bench, demonstrating the performance of landing gear electromechanical actuator controls under power system and load transients.

References

    1. 1)
      • 4. Baker, D.D., Mooney, D.P.: ‘Boeing 787–8 design, certification and manufacturing systems review’, Boeing 787–8 Critical Systems Review Team, 2014.
    2. 2)
      • 9. Todd, R., Forsyth, A., Lowe, V.: ‘Reconfigurable aircraft DC power networks laboratory’, SAE Technical Paper 2010-01-1782, 2010.
    3. 3)
      • 8. Todd, R., Forsyth, A.J.: ‘HIL emulation of all-electric UAV power systems’. 2009 IEEE Energy Conversion Congress and Exposition, San Jose, CA, USA, 2009, pp. 411416.
    4. 4)
      • 11. Habibi, S., Roach, J., Luecke, G.: ‘Inner-loop control for electromechanical (EMA) flight surface actuation systems’, J. Dyn. Syst. Meas. Contr., 2008, 130, pp. 051002051002-13.
    5. 5)
      • 13. Areerak, K.: ‘Modelling and stability analysis of aircraft power systems’. PhD thesis, University of Nottingham, 2009.
    6. 6)
      • 3. Rosero, J.A., Ortega, J.A., Aldabas, E., et al: ‘Moving towards a more electric aircraft’, IEEE Aerosp. Electron. Syst. Mag., 2007, 22, pp. 39.
    7. 7)
      • 2. Hale, J.: ‘Boeing 787 from the ground Up’, Boeing AERO Magazine, 2006, pp. 1523.
    8. 8)
      • 14. Gan, C., Todd, R., Apsley, J.: ‘Time-delay effects in a HIL aircraft power system emulator’. 2013 IEEE Energy Conversion Congress and Exposition, Denver, CO, USA, 2013, pp. 2026.
    9. 9)
      • 5. Karpenko, M., Sepehri, N.: ‘Hardware-in-the-loop simulator for research on fault tolerant control of electrohydraulic actuators in a flight control application’, Mechatronics, 2009, 19, (7), pp. 10671077.
    10. 10)
      • 15. Chakraborty, I.: ‘Subsystem Architecture Sizing and Analysis for Aircraft Conceptual Design’. PhD thesis, Georgia Institute of Technology, 2015.
    11. 11)
      • 16. Yerlikaya, U., Balkan, T.: ‘Dynamic modeling and control of an electromechanical control actuation system’. Presented at the ASME Dynamic Systems and Control Conf., Virginia, USA, 2017.
    12. 12)
      • 10. Correa, B.A., Zhang, Y., Fang, R., et al: ‘Driving a synchronous motor so that it emulates a twin-shaft gas turbine engine’. 6th IET Int. Conf. on Power Electronics, Machines and Drives (PEMD 2012), Bristol, UK, 2012, pp. 16.
    13. 13)
      • 1. Roboam, X., Sareni, B., Andrade, A.D.: ‘More electricity in the air: toward optimized electrical networks embedded in more-electrical aircraft’, IEEE Ind. Electron. Mag., 2012, 6, pp. 617.
    14. 14)
      • 12. Xin, Z., Guerrero, J.M., Xiaohua, W.: ‘Review of aircraft electric power systems and architectures’. 2014 IEEE Int. Energy Conf. (ENERGYCON), Cavtat, Croatia, 2014, pp. 949953.
    15. 15)
      • 6. Karpenko, M., Sepehri, N.: ‘Electrohydraulic force control design of a hardware-in-the-loop load emulator using a nonlinear QFT technique’, Control Eng. Pract., 2012, 20, (6), pp. 598609.
    16. 16)
      • 7. Griffo, A., Drury, D., Salt, D.: ‘Hardware in the loop based synchronous generator emulation test rig for more electric aircraft power systems’. 6th IET Int. Conf. on Power Electronics, Machines and Drives (PEMD 2012), Bristol, UK, 2012, pp. 16.
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