Methods of computer design technology ejection devices for missile aircraft of the fifth generation

Аuthors

Chemyakin A. V., Wroblewski E. G., Zaretsky D. M., Yudakov S. V.

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

Abstract

This work is devoted to simulation of aircraft armament robotic systems The analysis of technology market of mathematical modeling. For example, aircraft ejection systems for aircraft of the fifth generation of advanced technology research examined the kinematic and dynamic properties of complex linkage: the technology of solid-state models, measurement technologies of mass-dimensional characteristics, including tensor of moments of inertia of complex parts, and immediately the process of creating models of complex spatial mechanism with the subsequent investigation of its kinematics and dynamics. The work is the development of the technology of computer simulation, which permits a sufficiently adequate dynamic model of linkage with varying parameters and to measure position, velocity, acceleration of any of its points and the magnitude of reactions in the hinges at any time.

Keywords:

fifth generation fighter aircraft, the separation of cargo, aircraft ejection device modeling, solid-state model, dynamic model

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