Налаштування робастного ПІД-регулятора для невизначеної нелінійної динамічної моделі безпілотного літального апарату
DOI:
https://doi.org/10.18372/1990-5548.53.12143Ключові слова:
Робастний ПІД-регулятор, безпілотний літальний апарат, невизначений аеродинамічний коефіцієнт, лінійна і нелінійна невизначена динамічна модель, метод помилки щодо виходу, оптимізація, алгоритм імітації відпалу, літаюче крило.Анотація
Запропоновано двоетапну процедуру налаштування робастного ПІД-регулятора для невизначеної нелінійної динамічної системи безпілотного літального апарату на основі методу нелінійної оптимізації та помилки щодо виходу в тимчасовій області. Пропонована процедура використовується для налаштування робастного ПІД-регулятора моно-крила Skywalker X8 для каналів бічного і крену. Для оцінювання запропонованої процедури налаштування робастного ПІД-регулятора для каналів бічного і крену, також розроблений метод з використанням команди «systune» в програмному забезпеченні Matlab. Запонований метод, можна використовувати для синтезу робастного керування з відомими структурами для невизначених нелінійних систем.
Посилання
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