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Register a new userDesign of stabilization and guidance system for a quadrotor UAV
تصمیم نظام استقرار و توجیه لطائرة مسیرة رباعیة المراوح
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Publication date
2016
and research's language is
العربية
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تهدف هذه الدراسة إلى تصمیم نظام تحكم للمحافظة على استقرار الطائرة، و ذلك باستخدام حساس تسارع ثلاثي المحاور و حساس سرعة زاویة ثلاثي المحاور. كما تهدف للتعرف على الحوامات رباعیة المراوح، و اعتماد هذا البحث كقاعدة أساسیة ترتكز علیها أبحاثاً لاحقة حول مختلف التطبیقات لهذا النوع من الطائرات.
The focal point of this thesis is design of a control system to achieve the stability of the aircraft, by using a three-axis accelerometer sensor and a three-axis gyro. This thesis aims to studying the quadrotor UAV, and depend this research as a base for subsequent research on the various applications of this type of aircraft.
References used
J.G. Leishman. The Breguet-Richet Quad-Rotor Helicopter of 1907. Vertiflite, 47(3):1–4, 2001
W. Barnes and W. McCormick. Aerodynamics, Aeronautics and Flight Mechanics. New York: Wiley, 2nd. Edition, 1995
Gjioni E. AbouSleiman R., Korff D. and Yang H. The oakland university unmanned aerial quadrotor system. 2008
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