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Helicopter pilot model for pitch attitude tracking task (CROSBI ID 649320)

Prilog sa skupa u zborniku | izvorni znanstveni rad | međunarodna recenzija

Vrdoljak, Milan ; Viertler, Franz ; Hajek, Manfred ; Heller, Matthias Helicopter pilot model for pitch attitude tracking task // Proceedings of Euro GNC 2017 - 4th CEAS Specialist Conference on Guidance, Navigation & Control / Głębocki, Robert (ur.). Varšava: Warsaw University of Technology, 2017. str. 1-15

Podaci o odgovornosti

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

engleski

Helicopter pilot model for pitch attitude tracking 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.

model pilota, helikopter, zadaća slijeđenja propinjanja, eksperiment na simulatoru leta

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Podaci o prilogu

1-15.

2017.

objavljeno

Podaci o matičnoj publikaciji

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

Głębocki, Robert

Varšava: Warsaw University of Technology

Podaci o skupu

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

predavanje

25.04.2017-27.04.2017

Varšava, Poljska

Povezanost rada

Zrakoplovstvo, raketna i svemirska tehnika