Question 30-1 : Helicopter flight controls .the collective lever is so named because ? [ Students equipment ]

Question 1

Question 30-1 : Helicopter flight controls .the collective lever is so named because ? [ Students equipment ]

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

Answer

Wing span and mean chord line

Answer

The foremost edge of a wing

Answer

The rear edge of a wing

Answer

The straight line between the leading edge and the trailing edge

Question 2

Question 30-2 : Helicopter flight controls .to put into a forward flight motion a rpas helicopter ?

You have to tilt the main rotor plane of rotation ahead

Question 3

Question 30-3 : Helicopter flight controls .for a remotely piloted aircraft system rpas helicopter type tail rotor has the particular function to ?

Control the rotation of the airframe on the yaw axis

Question 4

Question 30-4 : Flight controls .rolling is the rotation of the aeroplane about the ?

Longitudinal axis

Question 5

Question 30-5 : Flight controls .rotation about the lateral axis is called ?

Pitching

Question 6

Question 30-6 : Flight controls .rotation around the longitudinal axis is called ?

Rolling

Question 7

Question 30-7 : Flight controls .rotation around the normal vertical axis is called ?

Yawing

Question 8

Question 30-8 : Design of the wing .aspect ratio of a wing is the ratio between ?

Question 9

Question 30-9 : Design of the wing .leading edge is ?

Question 10

Question 30-10 : Design of the wing .trailing edge is ?

Question 11

Question 30-11 : Define the term 'wing cord' ?

Question 12

Question 30-12 : Multi rotor aircraft dynamics .during a flight under gps stabilize mode your drone moves from its desired path your action is ?

I'm taking back manual flight control under attitude stabilized mode

Question 13

Question 30-13 : Multi rotor aircraft dynamics .as a multi rotor or a'helicopter' accelerates the attitude becomes ?

Nose down

Question 14

Question 30-14 : Multi rotor aircraft dynamics .for a remotely piloted aircraft system multi rotor type to yaw to the left or to the right ?

Engines located on the same axis must turn faster

Question 15

Question 30-1 : Helicopter flight controls .the collective lever is so named because ? [ Students equipment ]

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

Question 30-2 : Helicopter flight controls .to put into a forward flight motion a rpas helicopter ?

You have to tilt the main rotor plane of rotation ahead

Question 30-3 : Helicopter flight controls .for a remotely piloted aircraft system rpas helicopter type tail rotor has the particular function to ?

Control the rotation of the airframe on the yaw axis

Question 30-4 : Flight controls .rolling is the rotation of the aeroplane about the ?

Longitudinal axis

Question 30-5 : Flight controls .rotation about the lateral axis is called ?

Pitching

Question 30-6 : Flight controls .rotation around the longitudinal axis is called ?

Rolling

Question 30-7 : Flight controls .rotation around the normal vertical axis is called ?

Yawing

Question 30-8 : Design of the wing .aspect ratio of a wing is the ratio between ?

Wing span and mean chord line

Question 30-9 : Design of the wing .leading edge is ?

The foremost edge of a wing

Question 30-10 : Design of the wing .trailing edge is ?

The rear edge of a wing

Question 30-11 : Define the term 'wing cord' ?

The straight line between the leading edge and the trailing edge

Question 30-12 : Multi rotor aircraft dynamics .during a flight under gps stabilize mode your drone moves from its desired path your action is ?

I'm taking back manual flight control under attitude stabilized mode

Question 30-13 : Multi rotor aircraft dynamics .as a multi rotor or a'helicopter' accelerates the attitude becomes ?

Nose down

Question 30-14 : Multi rotor aircraft dynamics .for a remotely piloted aircraft system multi rotor type to yaw to the left or to the right ?

Engines located on the same axis must turn faster

Question 30-15 : Multi rotor aircraft dynamics .for a remotely piloted aircraft system multi rotor type to generate a roll to the right ?

Engines located on the right must be reduced