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العنوان
Attitude and altitude stabilization of Quad rotor /
الناشر
Tarek Naem Mohamed Deif ,
المؤلف
Tarek Naem Mohamed Deif
هيئة الاعداد
باحث / Tarek Naem Mohamed Deif
مشرف / Gamal Mahmoud El Bayoumi
مشرف / Ayman Hamdy Kassem
مناقش / Ayman Hamdy Kassem
مناقش / Magdi Osman Tantawy
تاريخ النشر
2014
عدد الصفحات
111 P. :
اللغة
الإنجليزية
الدرجة
ماجستير
التخصص
هندسة الطيران والفضاء
تاريخ الإجازة
1/1/2014
مكان الإجازة
جامعة القاهرة - كلية الهندسة - Aerospace
الفهرس
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Abstract

Quad rotor is a new class of the aerial unmanned aerial vehicles that could fly and stabilize its motion by couple of rotors that could hover and make a directional motion. Quad rotor has some advantages if we compared it with the helicopters; as it is compact, and has simple mechanical structure with high maneuverability. When the flight is dangerous, monotonous, or not possible even by a skilled pilot, an unmanned quad rotor can give successful results. As it can take-off and land in a limited area, and can easily hover above any target. Helicopters are very complex to study its model, and design the suitable controller which can stabilize them. In the helicopter study, we the pilot can{u201F}t make the control action to stabilize it as it{u201F}s very complex system; so the control design is responsible for taking the required action to stabilize the helicopter to the operating point. The pilot just gives helicopter the required input, and the controller deal with the system to achieve the input from pilot