RECONFIGURATION OF THE AIRCRAFT INTEGRATED CONTROL SYSTEM REGARDING CONTROL CONSTRAINTS UNDER ACTUATOR FAILURES

RECONFIGURATION OF THE AIRCRAFT INTEGRATED CONTROL SYSTEM REGARDING CONTROL CONSTRAINTS UNDER ACTUATOR FAILURES

The aircraft integrated control system reconfiguration laws under failures of actuators, calculated disregarding physical constraints on control surfaces saturation, can lead to a complete loss of aircraft controllability and stability. Despite the large number of scientific publications in this fie...

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Bibliographic Details
Main Authors: A. M. Kulchak, V. V. Kosyanchuk, E. Yu. Zybin
Format: Article
Language:Russian
Published: Moscow State Technical University of Civil Aviation 2018-12-01
Series:Naučnyj Vestnik MGTU GA
Subjects:
reconfiguration
integrated control system
actuator failures
control constraints
approximate pseudoinverse solution
reconfiguration power
reconfiguration error
Online Access:https://avia.mstuca.ru/jour/article/view/1404

Internet

https://avia.mstuca.ru/jour/article/view/1404

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