Account of elasticity in the flying machine kinematic control system

Author

Ghukasyan, Artush A. ; Hayrapetyan, Vahe V.

Author_Institution

Dept. of Mech., Yerevan State Univ., Armenia

Volume

1

fYear

2000

fDate

2000

Firstpage

84

Abstract

For one model of flying machine with elastic elements of type plates, within the framework of the linear theory of elasticity, are brought the equations of onward and rotational motions, as well as plates elastic oscillations equations. It is investigated the problem of cinematic control of program motion, which cybernetic scheme takes into account additional control forces and moments, stipulated by the elasticity of the construction. For different constructional materials of the plates are brought the results of numerical analysis of functioning of an additional regulator in the general control scheme

Keywords

aircraft control; elasticity; feedback; nonlinear dynamical systems; variational techniques; cinematic control; cybernetic scheme; elastic oscillations equations; elasticity; flying machine kinematic control system; numerical analysis; program motion; rotational motions; Centralized control; Control system synthesis; Control systems; Elasticity; Equations; Force control; Kinematics; Motion analysis; Motion control; Potential energy;

fLanguage

English

Publisher

ieee

Conference_Titel

Control of Oscillations and Chaos, 2000. Proceedings. 2000 2nd International Conference

Conference_Location

St. Petersburg

Print_ISBN

0-7803-6434-1

Type

conf

DOI

10.1109/COC.2000.873516

Filename

873516