The goal of this thesis is to identify airplanes’ reduced order transfer functions, and aerodynamic derivatives in the longitudinal channel. The outcome of the research will benefit aircraft systems’ controller design, modeling and simulation. To identify the system transfer functions and aerodynamic derivatives, direct and indirect frequency domain identification methods are applied. For the direct method, the Equation Error (EE) method is adopted to process the Cropcam’s input-output data pairs and identify the aerodynamic derivatives from the flight data directly. The indirect approach is called the Transfer Function (TF) method. The derivatives identified by the EE method and transfer function method are compared with the ones computed from a Vortex Lattice based program called AVL. The identification results are further verified by comparing computer simulation outputs with flight test responses.
| Identifer | oai:union.ndltd.org:MANITOBA/oai:mspace.lib.umanitoba.ca:1993/23942 |
| Date | 02 September 2014 |
| Creators | Xu, Kaiwen Jr |
| Contributors | Sepehri, Nariman (Mechanical Engineering) Bolandhemmat, Hamidreza (Mechanical Engineering), Kinsner, Witold (Electrical and Computer Engineering) Balakrishnan, S. (Mechanical Engineering) |
| Source Sets | University of Manitoba Canada |
| Detected Language | English |
Page generated in 0.0022 seconds