Flight Control Systems
Last updated
Last updated
The flight control systems consist of the and .
The rotor flight control systems consisting of cyclic, collective, and directional controls are used to adjust the helicopter attitude, altitude, and direction of flight. For a system discussion and/or description, refer to .
The hydraulic power system supplies pressurized fluid to operate the cyclic and collective flight control servo-actuators. Without the aid of hydraulic power, pilot effort to manually counteract the control feedback forces of the cyclic and collective flight controls is drastically increased. For a system discussion and/or description, refer to .