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