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Helicopter flight controls The «collective lever» is so named because ?

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exemple 30
It alters pitch of all main rotor blades at same time, it allows to invert pitch of all main rotor blades, it changes pitch of main tail rotor blades at same time, it increases or decreases rotational speed of rotors.

Helicopter flight controls To put into a forward flight motion a RPAS helicopter ?

exemple 31
Helicopter flight controls to put into a forward flight motion a rpas helicopter You have to tilt main rotor plane of rotation ahead, you have to tilt main rotor plane of rotation backwards, the tail rotor must generated a motion to right, the tail rotor must generated a motion to left.

Helicopter flight controls For a Remotely Piloted Aircraft System RPAS helicopter type tail rotor has the particular function to ?

exemple 32
Helicopter flight controls for a remotely piloted aircraft system rpas helicopter type tail rotor has particular function to Control rotation of airframe on yaw axis, increase available power the main rotor while hovering, allow lateral motions while hovering, allow control of flight around roll axis.

  • exemple 33
    Flight controls rolling the rotation of aeroplane about Longitudinal axis, vertical axis, lateral axis, wing axis.

  • exemple 34
    Flight controls rotation about lateral axis called Pitching, yawing, rolling, slipping.

  • exemple 35
    Flight controls rotation around longitudinal axis called Rolling, yawing, pitching, slipping.

  • exemple 36
    Flight controls rotation around normal vertical axis called Yawing, rolling, pitching, slipping.

  • Question Section 7: Theory of flight 30 Answer 8

    Design of wing aspect ratio of a wing the ratio between Wing span mean chord line, wing span dihedral angle, wing span wing root chord, wing root chord line wing tip chord line.

  • Question Section 7: Theory of flight 30 Answer 9

    Design of wing leading edge The foremost edge of a wing, the rear edge of a wing, the underside of wing, the tip of a wing.

  • Question Section 7: Theory of flight 30 Answer 10

    Design of wing trailing edge The rear edge of a wing, the underside of wing, the foremost edge of a wing, the tip of a wing.

  • Question Section 7: Theory of flight 30 Answer 11

    Define term 'wing cor The straight line between leading edge the trailing edge, the straight line between extrados the lower wing surface, the straight line between leading edge the upper wing surface, the straight line between trailing edge the upper wing surface.

  • Question Section 7: Theory of flight 30 Answer 12

    Multi rotor aircraft dynamics during a flight under «gps stabilize» mode your drone moves from its desired path your action I'm taking back manual flight control under attitude stabilized mode, i stop engines, i let it do, system will automatically come back to route, i reset my remote control unit.

  • Question Section 7: Theory of flight 30 Answer 13

    Multi rotor aircraft dynamics as a «multi rotor» or a'helicopter' accelerates attitude becomes Nose down, nose up, level, nose up or nose down depending on kind of aircraft.

  • Question Section 7: Theory of flight 30 Answer 14

    Multi rotor aircraft dynamics for a remotely piloted aircraft system multi rotor type to yaw to left or to right Engines located on same axis must turn faster, engines located on right must be reduced, engines located on left must be reduced, engines located at front must spin faster.

  • Question Section 7: Theory of flight 30 Answer 15

    Multi rotor aircraft dynamics for a remotely piloted aircraft system multi rotor type to generate a roll to right Engines located on right must be reduced, engines located on left must be reduced, engines located at front must spin faster, engines located at back must spin faster.


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