Sliding Mode Trajectory Tracking Control for a Quadrotor
عنوان مقاله: Sliding Mode Trajectory Tracking Control for a Quadrotor
شناسه ملی مقاله: AEROSPACE16_202
منتشر شده در شانزدهمین کنفرانس بین المللی انجمن هوافضای ایران در سال 1395
شناسه ملی مقاله: AEROSPACE16_202
منتشر شده در شانزدهمین کنفرانس بین المللی انجمن هوافضای ایران در سال 1395
مشخصات نویسندگان مقاله:
Kian Gheitasi - Faculty of New Sciences and Technologies, University of Tehran, Tehran, Iran MSc Student of Aerospace Engineering-University of Tehran
Mohammad Ali Amiri Atashgah - Faculty of New Sciences and Technologies, University of Tehran, Tehran, Iran Assistant Prof.,
خلاصه مقاله:
Kian Gheitasi - Faculty of New Sciences and Technologies, University of Tehran, Tehran, Iran MSc Student of Aerospace Engineering-University of Tehran
Mohammad Ali Amiri Atashgah - Faculty of New Sciences and Technologies, University of Tehran, Tehran, Iran Assistant Prof.,
This paper presents tracking control design for a quadrotor based on sliding mode method. Quadrotor is a kind of flying robots, which has six degrees of freedom. Because of its under-actuated dynamic property, the controller can make quadrotor to track roll, pitch and yaw angles and
کلمات کلیدی: Quadrotor - Sliding Mode Method - Controller - Tracking
صفحه اختصاصی مقاله و دریافت فایل کامل: https://civilica.com/doc/636563/