COMPLEX PROCESS OF ACTIVELY CONTROLLING AN AIRPLANE WING VIBRATIONS UPON TURBULENCE, BASED ON AN EMERGENT METHODOLOGY OF MATHEMATICAL MODEL IDENTIFICATION

The invention relates to a process for controlling airplane wing vibrations upon turbulence. According to the invention, the process determines a mathematical model of the wing, comprising the following sequence of operations: input of a temporal signal to a servo-actuator having the data of an appr...

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Bibliographische Detailangaben

Hauptverfasser:	ARGHIR MINODOR, ENCIU DANIELA, TOADER ADRIAN, STOICA CORNELIU IOAN, URSU IOAN, TECUCEANU GEORGE, GUŢĂ ION DRAGOŞ DANIEL, ANDREI DRAGOŞ, PEPELEA DUMITRU
Format:	Patent
Sprache:	eng ; rum
Schlagworte:	CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING FUNCTIONAL ELEMENTS OF SUCH SYSTEMS MEASURING MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS PHYSICS REGULATING TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR
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