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I have functions of the position v=v(x,y) , w=w(x,y), c=c(h) that I want to determine the air speed, rate of change in heading angle, and rate of change of altitude of a fixed wing UAV. I would like to simulate using thses controls using matlab simulink and UAV Toolbox
Autopilot control and justification (Non-GPS) Testing of VOR and ADF/NDB instruments (Non-GPS) Flight planning and GPS navigation techniques (GPS) Gas Turbine Engine Testing and Data Analysis documents will be attached separately upon request
Assessment format: a video recording of a numerical experiment with audio description Analyse an impact of change of an angle of attack on the aircraft trim parameters. Create a MATLAB script or a live script which reads all provided aircraft input data and calculate aircraft trim parameters for 3 selected angles of attack and constant altitude of your choice. The aircraft model must meet the f...
Testcase generation from C code