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Airplane Ground Collision Avoidance System Design Based on Optimal Tracking Control
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نویسنده
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Nikkhah Amirali ,Mojarrab Hoseyn ,Mojarrab Fatemeh ,Zardashti Reza
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منبع
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Journal Of Aerospace Science And Technology - 2021 - دوره : 14 - شماره : 2 - صفحه:106 -115
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چکیده
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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 3 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 discretetime linear quadratic tracker is designed, to fly over or pass obstacles like mountains automatically.
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کلیدواژه
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Automatic Flight Control System; Ground Collision Avoidance System; Linear Quadratic Tracker; Digital Image Processing; Optimal Control System
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آدرس
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K.N. Toosi University Of Technology, Aerospace Department, Iran, K.N. Toosi University Of Technology, Aerospace Department, Iran, Islamic Azad University, Qazvin Branch, Electrical Engineering Department, Iran, Malek-Ashtar University Of Technology, Aerospace Department, Iran
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Airplane Ground Collision Avoidance System Design based on Optimal Tracking Control
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Authors
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Abstract
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Keywords
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