Summary
Daqing Yang is a Teaching Fellow at the Department of Aeronautics. His teaching interest covers aircraft conceptual design, airframe preliminary design, flight mechanics and aerospace project development.
His research interest is focused on aircraft configuration development with the aid of flight simulation. He is experienced in aircraft concept validation by means of scaled flight experiment.
Background
2020 - present: Teaching Fellow in the Department of Aeronautics at Imperial College London.
2018 - 2019: Research Fellow in Aerospace Integration Research Centre (AIRC) at Cranfield University.
2012 - 2017: Research and Development engineer in Beijing Aeronautical Science and Technology Research Institute of COMAC.
2007 - 2011: PhD in Aerospace Engineering at Cranfield University, UK. Thesis title "Stability and control of seamless aeroelastic wing aircraft".
2002 - 2006: BEng in Aerospace System Engineering at University of Hertfordshire, UK.
Selected Publications
Journals
D.Li, S.Guo, D.Yang, et al. 2016, Active control design for an unmanned air vehicle with a morphing wing, Aircraft Engineering and Aerospace Technology. ISSN 1748-8842. DOI
Wang Z, Yang D & Guo S, 2009, Rolling active control for an
aircraft of seamless aeroelastic wing, International Journal of
Modelling, Identification and Control, 7 (3) 225 233. DOI
Conference
Z.Wang, Y.Sun, D.Yang, S.Guo. 2012, Active control using control allocation for UAVs with seamless morphing wing, Third international conference on Smart materials and Nanotechnology in Engineering, SPIE. DOI
D.Li, S.Guo, N.Matteo, D.Yang, 2011, Design, experiment and aerodynamic calculation of a flapping wing rotor micro aerial vehicle, 52nd Structures, structural dynamics and materials conference, AIAA. DOI