Helicopter Pilot Model for Pitch Attitude Track Task (CROSBI ID 60747)
Prilog u knjizi | izvorni znanstveni rad | međunarodna recenzija
Podaci o odgovornosti
Vrdoljak, Milan ; Viertler, Franz ; Hajek, Manfred ; Heller, Matthias
engleski
Helicopter Pilot Model for Pitch Attitude Track Task
A helicopter pilot model as a part of the pilot-vehicle system is analyzed for the task of pitch attitude tracking in forward flight. Analytical helicopter pilot model, following the Efremov’s modification of the structural model, is defined through the optimization algorithm based on the minimum of the error variance. A set of the pilot-in-the-loop experiments were conducted at the research helicopter flight simulator with a fixed base and high fidelity visual system. In these experiments pilots were given different pitch commands visually at the primary flight display and the helicopter’s resulting pitch attitude was recorded. These results from the flight simulator experiments were used for the comparison with the results of the pilot-vehicle system with the defined analytical pilot model.
pilot model, helicopter, pitch tracking task, flight simulator experiment
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Podaci o prilogu
225-239.
objavljeno
10.1007/978-3-319-65283-2_12
Podaci o knjizi
Advances in Aerospace Guidance, Navigation and Control
Dołęga, B. ; Głębocki, R. ; Kordos, D. ; Żugaj, M.
Cham: Springer
2018.
978-3-319-65282-5
Povezanost rada
Zrakoplovstvo, raketna i svemirska tehnika