Helicopter flight controls The cyclic control stick on a helicopter ?

Name: Examen answer,73 session uav
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exemple 86 — Changes pitch of rotor blades independently to create directional control, tilts tail rotor forwards or backwards, increases pitch of tail rotor blades to create thrust, decreases pitch of tail rotor blades to create thrust.

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

exemple 87 — Helicopter flight controls the 'collective lever' so named because 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 88 — 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 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.
Flight controls rolling the rotation of aeroplane about Longitudinal axis, vertical axis, lateral axis, wing axis.
Flight controls rotation about lateral axis called Pitching, yawing, rolling, slipping.
Flight controls rotation around longitudinal axis called Rolling, yawing, pitching, slipping.
Question Section 7: Theory of flight 73 Answer 8

Flight controls rotation around normal vertical axis called Yawing, rolling, pitching, slipping.
Question Section 7: Theory of flight 73 Answer 9

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 73 Answer 10

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 73 Answer 11

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 73 Answer 12

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 73 Answer 13

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 73 Answer 14

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 73 Answer 15

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.