How do civil aviation planes operate? Where are the power supply and joystick?

When you roll over, you control the aileron of the aircraft to control the tilt of the aircraft. When pulling back or pushing forward, it is to control the elevator of the aircraft and control the pitch of the aircraft, that is, to look up and down. There is also the pedal, which is similar to the position of the automobile accelerator brake. This is to control the rudder of the plane, that is, to control the direction of the plane.

If the altitude is the altitude when the plane takes off or lands, the flaps will be lowered to increase the lift or resistance. After cruising, the elevator will be controlled to adjust the height of the aircraft. Yawing is to control the rudder. In order to distinguish between turning and yaw, all aircraft are equipped with autopilot, which will automatically distinguish.

The throttle lever is two white bars in the middle position, push forward. Left and right hair control, usually push together.

Joysticks are the two black ones that can be seen. The one on the left belongs to the captain and the one on the right belongs to the co-pilot. They are connected.

Extended data:

The main control system is used to control the flight trajectory and attitude of the aircraft, and consists of elevator (or full-moving horizontal tail), aileron, rudder and other control mechanisms.

The system should let the driver feel the change of displacement and force, which is the main difference from the auxiliary control system. The auxiliary control system includes wing, flap, speed brake, adjustable stabilizer and wing variable sweep angle control mechanism. Their operation can only be completed by selecting the corresponding switch position and turning on the motor or hydraulic actuator through electrical signals.

The control instructions of the automatic control system come from the sensors of the system, which can automatically respond to external disturbances to maintain the specified flight state and improve the flight quality of the aircraft. Commonly used automatic control systems include autopilot, various stability augmentation systems, automatic landing systems and active control systems.

The work of the automatic control system and the driver's manipulation are independent and do not interfere with each other. The main control system of aircraft has experienced a development process from simple primary to complex and perfect. Mechanical control, reversible and irreversible power-assisted control and fly-by-wire control have appeared successively, and active control technology has been developed on the basis of fly-by-wire control.

Baidu Encyclopedia-Aircraft Control System