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Helicopter flight controls the cyclic control stick on a helicopter ? [ Session UAV ]

Question 73-1 : Changes the pitch of the rotor blades independently to create directional control tilts the tail rotor forwards or backwards increases the pitch of the tail rotor blades to create thrust decreases the pitch of the tail rotor blades to create thrust

exemple 73 Changes the pitch of the rotor blades independently to create directional control.Changes the pitch of the rotor blades independently to create directional control.

Helicopter flight controls the 'collective lever' is so named because ?

Question 73-2 : It alters the pitch of all main rotor blades at the same time it allows to invert the pitch of all the main rotor blades it changes the pitch of the main and tail rotor blades at the same time it increases or decreases the rotational speed of the rotors

exemple 77 It alters the pitch of all main rotor blades at the same time.It alters the pitch of all main rotor blades at the same time.

Helicopter flight controls to put into a forward flight motion a rpas helicopter ?

Question 73-3 : You have to tilt the main rotor plane of rotation ahead you have to tilt the main rotor plane of rotation backwards the tail rotor must generated a motion to the right the tail rotor must generated a motion to the left

exemple 81 You have to tilt the main rotor plane of rotation ahead.You have to tilt the main rotor plane of rotation ahead.

Helicopter flight controls for a remotely piloted aircraft system rpas ?

Question 73-4 : Control the rotation of the airframe on the yaw axis increase available power for the main rotor while hovering allow lateral motions while hovering allow the control of the flight around the roll axis

exemple 85 Control the rotation of the airframe on the yaw axis.Control the rotation of the airframe on the yaw axis.

Flight controls rolling is the rotation of the aeroplane about the ?

Question 73-5 : Longitudinal axis vertical axis lateral axis wing axis

exemple 89 Longitudinal axis.Longitudinal axis.

Flight controls rotation about the lateral axis is called ?

Question 73-6 : Pitching yawing rolling slipping

exemple 93 Pitching.Pitching.

Flight controls rotation around the longitudinal axis is called ?

Question 73-7 : Rolling yawing pitching slipping

exemple 97 Rolling.Rolling.

Flight controls rotation around the normal vertical axis is called ?

Question 73-8 : Yawing rolling pitching slipping

exemple 101 Yawing.Yawing.

Design of the wing aspect ratio of a wing is the ratio between ?

Question 73-9 : Wing span and mean chord line wing span and dihedral angle wing span and wing root chord wing root chord line and wing tip chord line

exemple 105 Wing span and mean chord lineWing span and mean chord line

Design of the wing leading edge is ?

Question 73-10 : The foremost edge of a wing the rear edge of a wing the underside of the wing the tip of a wing

exemple 109 The foremost edge of a wing.The foremost edge of a wing.

Design of the wing trailing edge is ?

Question 73-11 : The rear edge of a wing the underside of the wing the foremost edge of a wing the tip of a wing


Define the term 'wing cord' ?

Question 73-12 : The straight line between the leading edge and the trailing edge the straight line between the extrados and the lower wing surface the straight line between the leading edge is the upper wing surface the straight line between the trailing edge and the upper wing surface

exemple 117 The straight line between the leading edge and the trailing edge.The straight line between the leading edge and the trailing edge.

Multi rotor aircraft dynamics during a flight under 'gps stabilize' mode your ?

Question 73-13 : I'm taking back manual flight control under attitude stabilized mode i stop the engines i let it do the system will automatically come back to the route i reset my remote control unit


Multi rotor aircraft dynamics as a 'multi rotor' or a'helicopter' accelerates ?

Question 73-14 : Nose down nose up level nose up or nose down depending on the kind of aircraft


Multi rotor aircraft dynamics for a remotely piloted aircraft system multi ?

Question 73-15 : Engines located on the same axis must turn faster engines located on the right must be reduced engines located on the left must be reduced engines located at the front must spin faster



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