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dc.contributor.author |
Saada, Nourhane |
|
dc.contributor.author |
Chegrani, Ahmed (promoteur) |
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dc.date.accessioned |
2022-04-26T08:59:40Z |
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dc.date.available |
2022-04-26T08:59:40Z |
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dc.date.issued |
2021 |
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dc.identifier.uri |
http://di.univ-blida.dz:8080/jspui/handle/123456789/15665 |
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dc.description |
Mémoire de Master option Avionique.-Numéro de Thèse 083/2021 |
fr_FR |
dc.description.abstract |
This thesis presents within the framework of a conceptual context simulation of our F-16 fighter aircraft model using the MATLAB/Simulink environment. A theoretical study on theaircraft F-16 will be presented in which a mathematical model was obtained using NewtonEuler formulism. The non-linear model was linearized and decoupled for both longitudinaland lateral directions around equilibrium points at certain trim conditions to obtain statespace models. This work aims at a complete study, analysis, design and performancemonitoring of the classical (LQR, PID, FLC) and the new robust generation controllers (Selftuning Fuzzy PID, GA-PID, 𝐻2/𝐻∞) in terms of flight trajectory reference tracking andstability augmentation of the pitch motion. From the results achieved a comparative analysiswill be investigated. |
fr_FR |
dc.language.iso |
en |
fr_FR |
dc.publisher |
Université Blida 01 |
fr_FR |
dc.subject |
Non-linear/linear models;
Simulation;
Classical/robust controllers;
Stability;
Pitch motion |
fr_FR |
dc.title |
Enhancing the stabilization of the F-16 fighter aircraft pitch motion control via intelligent and classical method |
fr_FR |
dc.type |
Thesis |
fr_FR |
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