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Dynamics of non-autonomous spatial motion of an aeroplane with a deformable control system. (Polish. English, Russian summaries) Zbl 0606.73075

Spatial-motion dynamics was studied of an aircraft with deformable controls and movable ponderable control surfaces (ailerons, elevator and rudder) in the case of external forces in the form of pulses acting upon the aircraft in a finite time interval. A full nonlinear set of equations of the aircraft spatial motion was employed along with the equations of motion of the ailerons, the elevator and the rudder on consideration of external actions explicitly time-dependent. A program was prepared for numerical integration of the equations by the Runge-Kutta-Gill method.

MSC:

74H45 Vibrations in dynamical problems in solid mechanics
70Q05 Control of mechanical systems
74E30 Composite and mixture properties
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