Algorithms for Controlling Fatigue Tests of Airplanes
V. L. Prisekin, N. V. Pustovoi, G. I. Rastorguev
Novosibirsk State Technical University, Novosibirsk, 630073 Russia
Keywords: airplane, wing, modeling, system of force control, test program
Abstract
The efficiency of algorithms for automatic control of forces prescribed in the test program is analyzed by an example of a large-aspect-ratio wing considered as a beam loaded by aerodynamic and inertial forces.
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