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In order to understand this problem, let's first explain the motion of the aircraft. The aircraft moves around three axes: the horizontal axis (pitch), the vertical axis (roll), and the vertical axis (yaw).
1) Transverse axis (pitch): An imaginary straight line from the tip of one wing to the tip of the other wing. The motion of the aircraft around the horizontal axis is called pitching. Controlled by an elevator.
2) Longitudinal axis (roll): An imaginary straight line from the head to the tail of the aircraft. The movement of the aircraft around the longitudinal axis is called roll and is controlled by the ailerons.
3) Vertical axis (yaw): An imaginary straight line extending vertically from the intersection of the horizontal axis and the vertical axis. The movement of the aircraft around the vertical axis is called yaw and is controlled by the rudder.
An airplane can move around only one of the axes or all three at the same time.
In the case of military aircraft, for example, the elevator of the aircraft is operated by the forward and backward movement of the pilot's steering stick, and the rudder is operated by the left and right deflection of the pedals. The ailerons of the aircraft control the left and right deflection, and the pilot controls it by moving the steering stick left and right.
The above is a relatively simple statement, in fact, with the development of computer and fly-by-wire technology, the control of flight attitude will not be completed by a single rudder surface change, such as a downward dive, you can use ailerons and horizontal tail to change at the same time, so that the aircraft can achieve attitude changes faster and more smoothly. For pilots, it's also just a matter of pressing the steering stick forward. The change of the rudder surface is calculated and manipulated by the computer.
And the assumption you're talking about is basically impossible, because the electronic control system is very advanced today.
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Upstairs is right.
The wing is controlled by a hydraulic system.
That is, when your engine is down, you can still control the flight posture through the hydraulic transmission without the intervention of external forces.
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In the gliding state, as long as the rudder of the vertical tail can control the direction. The upper and lower rudders of the wings can control the balance of the fuselage from side to side.
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The wings are hydraulic, so you can use the steering wheel if you turn off in the middle of the drive.
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The wing is controlled by the hydraulic system, that is to say, when your engine is stopped, you can still control the flight posture through the hydraulic transmission, no external force is required, as long as the oil pressure (here refers to the hydraulic oil, not aviation gasoline) is normal, it will not be uncontrollable, hope to adopt!!
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