000			02246cam a2200337 a 4500
003			EG-GiCUC
005			20250223031216.0
008			150418s2014 ua dh f m 000 0 eng d
040			_aEG-GiCUC _beng _cEG-GiCUC
041	0		_aeng
049			_aDeposite
097			_aM.Sc
099			_aCai01.13.01.M.Sc.2014.Ta.A
100	0		_aTarek Naem Mohamed Deif
245	1	0	_aAttitude and altitude stabilization of Quad rotor / _cTarek Naem Mohamed Deif ; Supervised Gamal Mahmoud Elbayoumi , Ayman Hamdy Kassem
246	1	5	_aالتحكم فى زوايا وارتفاع مركبة طائرة باربعة مراوح
260			_aCairo : _bTarek Naem Mohamed Deif , _c2014
300			_a111 P. : _bcharts , facsimiles ; _c30cm
502			_aThesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering
520			_aQuad 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
530			_aIssued also as CD
653		4	_aGyroscopic effect
653		4	_aQuad rotor
653		4	_aUAV
700	0		_aAyman Hamdy Kassem , _eSupervisor
700	0		_aGamal Mahmoud Elbayoumi , _eSupervisor
856			_uhttp://172.23.153.220/th.pdf
905			_aNazla _eRevisor
905			_aSoheir _eCataloger
942			_2ddc _cTH
999			_c50497 _d50497