The influence of flight controls on aircraft's equations of motion
Theoretical and applied mechanics, Tome 6 (1980) no. 1, p. 123
The influence of flight commands on the differential equations of motion of the aircraft was considered using the Boltzmann-Hamel equations for holonomic systems. It has been shown that even for the case of constant relative control velocities, a more complete system of differential equations of aircraft motion is obtained, which between . it also takes gyroscopic influences into account.
@article{TAM_1980_6_1_a10,
author = {Gorazd Paljaruci},
title = {The influence of flight controls on aircraft's equations of motion},
journal = {Theoretical and applied mechanics},
pages = {123 },
year = {1980},
volume = {6},
number = {1},
language = {en},
url = {http://geodesic.mathdoc.fr/item/TAM_1980_6_1_a10/}
}
Gorazd Paljaruci. The influence of flight controls on aircraft's equations of motion. Theoretical and applied mechanics, Tome 6 (1980) no. 1, p. 123 . http://geodesic.mathdoc.fr/item/TAM_1980_6_1_a10/