HoverCore Flight Control System Operation Manual

System Overview

This is a flight control system that supports translational motion and attitude rotation control of the aircraft.

Basic Operation Instructions

Translational Control (Position Movement)

• Forward/Backward Translation: Controls the aircraft's forward/backward movement
• Up/Down Translation: Controls the aircraft's vertical ascent/descent
• Left/Right Translation: Controls the aircraft's lateral (side-to-side) movement

Control Logic: AG1 can switch between velocity control or acceleration control. The three axes correspond to target velocity or target acceleration, respectively.

Attitude Control (Rotation)

• Pitch: Controls the up/down tilt of the nose
• Roll: Controls the left/right tilt of the fuselage
• Yaw: Controls the left/right turning of the nose

Control Logic: Rotates around the three axes at a target angular velocity.

Braking System

• Brake: Brakes with a relatively high acceleration

Parameter Settings Explanation

Adjustable Parameters

• Maximum Acceleration (ACC_MAX): Limits the maximum acceleration during translational motion of the aircraft. Set by Slider1.
• Maximum Velocity (V_MAX): Limits the maximum velocity during translational motion of the aircraft (Velocity Control Mode only). Set by Throttle.
• Maximum Rotation Angular Velocity (K_A): Limits the maximum angular velocity during rotation of the aircraft. Set by Slider2.

Fixed Parameters

• Pitch Control Force (PAP): Control response strength for the Pitch axis. Set value: 10.
• Roll Control Force (PAR): Control response strength for the Roll axis. Set value: 10.
• Yaw Control Force (PAY): Control response strength for the Yaw axis. Set value: 10.

Note: The PAP/R/Y parameters control the magnitude of the control force for each rotation axis. A larger value results in a stronger torque generated for the same input.

When using the core, please place it at the center of gravity to better balance the thrust.