ISSN 1991-2927
 

ACP № 2 (56) 2019

Author: "Aleksandr Vitalevich Grebenkin"

Aleksandr Vitalevich Grebenkin, Marshal Bugaev Ulyanovsk Civil Aviation Institute, Professor at the Department of Flight Operation and Safety; graduated from the Lenin Komsomol Riga Institute of Civil Aviation Engineers; an author of articles and inventions in the field of flight safety and automated control of flight and thrust. [e-mail: grebenkin58@mail.ru]A. Grebenkin,

Aleksandr Aleksandrovich Lushnikov, Federal Research-and-Production Center Joint Stock Company ‘Research-and-Production Association ‘Mars’, Postgraduate Student at Marshal Bugaev Ulyanovsk Civil Aviation Institute; graduated from Radioengineering Faculty of Ulyanovsk State Technical University; Deputy Chief Designer at Federal Research-and-Production Center Joint Stock Company ‘Research-and-Production Association ‘Mars’. [e-mail: a.lushnikov@mail.ru]A. Lushnikov,

Vladimir Nikolaevich Moiseev, Federal Research-and-Production Center Joint Stock Company ‘Research-and-Production Association ‘Mars’, Candidate of Engineering; graduated from the Faculty of Economics and Mathematics of Ulyanovsk State Technical University; Software Engineer of the R&D Laboratory at Federal Research-and-Production Center Joint Stock Company ‘Research-and-Production Association ‘Mars’; an author of articles and inventions in the field of computer-aided facilities for naval and aeronautical engineering control. [e-mail: v.n.moiseev@mail.ru]V. Moiseev

Adaptive Stabilization and Tracking of Specified Flight Altitude and Speed 000_2.pdf

The article considers simulation of using additional signals of the system of automated control of flight and thrust in the section of spoilers (lifting strength and engine thrust control) in combination with control signals on a diving-rudder and control of engine thrust by a pilot of the system. In aid of research, the model of creating control signal on a diving-rudder and sections of spoilers of an aircraft in order to specify parameters of a control surface was simulated in MATLAB program with the use of Simulink package. The created models allows to get data about influence of adaptive method of flight speed control on parameters of tracking and stabilization of the specified indicated speed of an aircraft under conditions of wind shear, in breaking mode in forward flight, stabilization of the specified flight altitude in comparison with using of additional signal on spoilers and without using it. The obtained model allows to select necessary parameters for the specific control object at the initial stage of development promptly.

Adaptive stabilization, auto throttle, diving-rudder.

2017_ 3

Sections: Automated control systems

Subjects: Automated control systems, Mathematical modeling.


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