Robust Variable Structure Dynamic Sliding Mode Control of VTOL Aircraft
عنوان مقاله: Robust Variable Structure Dynamic Sliding Mode Control of VTOL Aircraft
شناسه ملی مقاله: ICESAL01_146
منتشر شده در کنفرانس بین المللی علوم مهندسی، هنر و حقوق در سال 1394
شناسه ملی مقاله: ICESAL01_146
منتشر شده در کنفرانس بین المللی علوم مهندسی، هنر و حقوق در سال 1394
مشخصات نویسندگان مقاله:
Erfan Arefi - Young Researchers and Elite Club, Sirjan branch, Islamic Azad University, Sirjan, Iran
خلاصه مقاله:
Erfan Arefi - Young Researchers and Elite Club, Sirjan branch, Islamic Azad University, Sirjan, Iran
In this paper, a design of autopilot for a Vertical Take-Off and Landing (VTOL) aircraft to track a predetermined desired flight path is examined. This system is a nonlinear non-minimum phase system. Since this aircraft faces to external distributions (e.g. wind) in flight, so designing of a controller with robust performance is critical to achievean optimal flight performance, despite presence of the external distributions. For this purpose, the dynamic sliding mode technique which is a robust method in the controller designing for nonlinear systems with uncertainties is used. By using the above method, the autopilot control law is designed in such a way that the aircraft tracksthe predetermined optimal paths (which are determined on type of aircraft missions). Simulations show effectiveness of the proposed control law
کلمات کلیدی: VTOL aircraft, dynamic sliding mode control, robust control
صفحه اختصاصی مقاله و دریافت فایل کامل: https://civilica.com/doc/388567/