Результаты исследований: Публикации в книгах, отчётах, сборниках, трудах конференций › статья в сборнике материалов конференции › научная
Helicopter autopilot based on precise nonlinear equations of the main rotor with Hiller hub. / Barabanov, A.E.
Proceedings of the 6th European Conference for Aerospace Sciences. 2015.Результаты исследований: Публикации в книгах, отчётах, сборниках, трудах конференций › статья в сборнике материалов конференции › научная
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TY - GEN
T1 - Helicopter autopilot based on precise nonlinear equations of the main rotor with Hiller hub
AU - Barabanov, A.E.
PY - 2015
Y1 - 2015
N2 - A cross influence between the blade pitch angle and the servo blade flapping angle is studied. A full mechanical equations of a rigid body motion was taken as a basis for a description of the flapping motion process. It was found that the dimensionless variables in the equations can be divided into groups by their decimal orders. The equations were truncated up to the second order of approximation error.
AB - A cross influence between the blade pitch angle and the servo blade flapping angle is studied. A full mechanical equations of a rigid body motion was taken as a basis for a description of the flapping motion process. It was found that the dimensionless variables in the equations can be divided into groups by their decimal orders. The equations were truncated up to the second order of approximation error.
M3 - Conference contribution
BT - Proceedings of the 6th European Conference for Aerospace Sciences
ER -
ID: 4749617