Manual

Table Of Contents
Chapter 1 Aircraft 11
EVO Max 4T User Manual
Figure 1-10 Install the Connector and fix the Connector Protective Cover
1.3 Flight Control System
EVO Max 4T achieves stable and convenient flight control through its built-in intelligent
flight control system. The system supports a number of advanced functions, including
return-to-home, failsafe, visual positioning system, etc.
Table 1-8 Flight Control System
Module Description
IMU
A three-axis gyroscope and a three-axis accelerometer measure
acceleration and angular velocity.
Compass
Measures the Earth's magnetic field and provides a heading
reference for the aircraft.
GNSS Receiver
Receive global satellite navigation signals to measure longitude,
latitude, and altitude.
Barometer
Measures atmospheric pressure and is used to determine the
altitude of the aircraft.
Binocular Visual
Perception System
Provide the aircraft with 720° obstacle awareness around the
fuselage.
Millimeter Wave Radar
Provide the aircraft with all-day and all-weather obstacle
avoidance capabilities.
1.3.1 Flight Modes
Depending on the availability of GNSS signals and flight conditions, the aircraft can