Airplane Ground Collision Avoidance System Design based on Optimal Tracking Control
عنوان مقاله: Airplane Ground Collision Avoidance System Design based on Optimal Tracking Control
شناسه ملی مقاله: JR_JASTI-14-2_009
منتشر شده در در سال 1400
شناسه ملی مقاله: JR_JASTI-14-2_009
منتشر شده در در سال 1400
مشخصات نویسندگان مقاله:
Amirali Nikkhah - Department of Aerospace engineering KNTU.ac.ir
Hoseyn Mojarrab - Department of Aerospace Engineering. KNTU.ac.ir
Fatemeh Mojarrab - Electrical Engineering Department ۰۳۹; Qazvin Islamic Azad University
Reza Zardashti - Aerospace Department Malek-Ashtar university of Technology
خلاصه مقاله:
Amirali Nikkhah - Department of Aerospace engineering KNTU.ac.ir
Hoseyn Mojarrab - Department of Aerospace Engineering. KNTU.ac.ir
Fatemeh Mojarrab - Electrical Engineering Department ۰۳۹; Qazvin Islamic Azad University
Reza Zardashti - Aerospace Department Malek-Ashtar university of Technology
The design of a ground collision avoidance system for an airplane based on optimal control theory is presented in this paper. A control system is designed by linear quadratic tracker to track desired Euler angles of airplane. The system independent of ۳ dimensional maps, works by using a forward looking camera. In addition, the obstacle is analyzed by digital image processing techniques. An optimal flight control system based on discrete-time linear quadratic tracker is designed, to fly over or pass obstacles like mountains automatically.
کلمات کلیدی: Automatic Flight Control System, Ground Collision Avoidance System, Linear quadratic tracker, Digital Image Processing, optimal control system
صفحه اختصاصی مقاله و دریافت فایل کامل: https://civilica.com/doc/1706337/