The influence of flight controls on aircraft's equations of motion
Theoretical and applied mechanics, Tome 6 (1980) no. 1, p. 123 .

Voir la notice de l'article provenant de la source eLibrary of Mathematical Institute of the Serbian Academy of Sciences and Arts

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.
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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/