Naslov
Helicopter pilot model for pitch attitude tracking task

Autori
Vrdoljak, Milan ; Viertler, Franz ; Hajek, Manfred ; Heller, Matthias

Vrsta, podvrsta i kategorija rada
Radovi u zbornicima skupova, cjeloviti rad (in extenso), znanstveni

Izvornik
Proceedings of Euro GNC 2017 - 4th CEAS Specialist Conference on Guidance, Navigation & Control / Głębocki, Robert - Varšava : Warsaw University of Technology, 2017, 1-15

Skup
Euro GNC 2017 - 4th CEAS Specialist Conference on Guidance, Navigation & Control

Mjesto i datum
Varšava, Poljska, 25.04.2017. - 27.04.2017

Vrsta sudjelovanja
Predavanje

Vrsta recenzije
Međunarodna recenzija

Ključne riječi
pilot model, helicopter, pitch tracking task, flight simulator experiment
(model pilota, helikopter, zadaća slijeđenja propinjanja, eksperiment na simulatoru leta)

Sažetak
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.

Izvorni jezik
Engleski

Znanstvena područja
Zrakoplovstvo, raketna i svemirska tehnika

POVEZANOST RADA