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.