Експериментальне дослідження інтегрованих навігаційних систем в задачах відстеження траєкторій квадрокоптерів
DOI:
https://doi.org/10.18372/1990-5548.73.17016Ключові слова:
глобальна навігаційна супутникова система, інерціальна навігаційна система, система наведення та управління, квадротор, експериментальні дослідження, льотні випробуванняАнотація
У статті представлено результати експериментальних досліджень інтегрованої системи навігації, наведення та керування квадрокоптера. Представлені математичні основи дослідження системи. Представлено алгоритм функціонування інтегрованої системи. Наведено рівняння оптимального оцінювання. Описано особливості експериментального обладнання. Змодельована траєкторія квадрокоптера в горизонтальній площині. Досліджено координати топоцентричної системи координат. Наведено результати експериментальних досліджень. Представлені компоненти швидкості. Наведено графічні залежності кутів рискання, тангажу та крену. Отримані результати можуть бути корисними для створення перспективних навігаційних систем для квадрокоптерів. Вони дозволяють підвищити якість їх навігації.
Посилання
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