1. A low cost model aircraft flight research facility in wind tunnel
- Author
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Nie, B., Guo, L., Cen, F., Olivier SENAME, Dugard, L., College of Intelligence Science and Engineering, National University of Defense Technology, China Aerodynamics Research and Development Center (CARDC), GIPSA - Systèmes linéaires et robustesse (GIPSA-SLR), Département Automatique (GIPSA-DA), Grenoble Images Parole Signal Automatique (GIPSA-lab ), Institut polytechnique de Grenoble - Grenoble Institute of Technology (Grenoble INP )-Institut Polytechnique de Grenoble - Grenoble Institute of Technology-Centre National de la Recherche Scientifique (CNRS)-Université Grenoble Alpes [2016-2019] (UGA [2016-2019])-Institut polytechnique de Grenoble - Grenoble Institute of Technology (Grenoble INP )-Institut Polytechnique de Grenoble - Grenoble Institute of Technology-Centre National de la Recherche Scientifique (CNRS)-Université Grenoble Alpes [2016-2019] (UGA [2016-2019])-Grenoble Images Parole Signal Automatique (GIPSA-lab ), and Institut polytechnique de Grenoble - Grenoble Institute of Technology (Grenoble INP )-Institut Polytechnique de Grenoble - Grenoble Institute of Technology-Centre National de la Recherche Scientifique (CNRS)-Université Grenoble Alpes [2016-2019] (UGA [2016-2019])-Institut polytechnique de Grenoble - Grenoble Institute of Technology (Grenoble INP )-Institut Polytechnique de Grenoble - Grenoble Institute of Technology-Centre National de la Recherche Scientifique (CNRS)-Université Grenoble Alpes [2016-2019] (UGA [2016-2019])
- Subjects
flight control law ,virtual flight test ,dynamic scaling ,wind tunnel ,ComputerApplications_COMPUTERSINOTHERSYSTEMS ,[SPI.AUTO]Engineering Sciences [physics]/Automatic - Abstract
International audience; This paper presents the overview of a low cost, generic aircraft model flight research facility housed in a wind tunnel at the Low Speed Aeronautics Institution (LSAI) of China Aerodynamics Research and Development Center (CARDC). It offers a cost effective way to investigating flight dynamics and evaluating designed control laws. First, the purpose and characteristics of the facility are described, alongside the description of the 3-DOF maneuver rig, dynamically scaled design and avionic system. The effectiveness of the proposed low-cost experimental facility is demonstrated via simulations and the virtual flight test involving a sub-scaled aircraft model with a scenario of performing conventional maneuvers.
- Published
- 2018