Owner manual
Guilin Feiyu Electronic Technology Co., Ltd.
Guilin Feiyu Electronic Technology Co., Ltd http://www.feiyu-tech.com service@feiyu-tech.com
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FY-DOS Manual For Multi-rotors Control
Installation & Operation Multi-rotor firmware above V2.20
Dear Customer:
Thank you for choosing DOS as your autopilot system. Please read this manual carefully before using
the system to ensure proper use and operation.
The installation and use of this device require some skill and knowledge in flying remote controlled
airplane model.
If you are a complete beginner and have never flown one before, we do not recommend you install
this device on your own.
Please find assistance from an experienced RC pilot who may provide you with the basic knowledge
required to use this device successfully.
If you are already an experienced flyer, you will find the DOS installation to be easy and logical. Just
follow this manual and you won’t go wrong.
If you need any technical support you can send e-mail directly to: service@feiyu-tech.com
DOS Module
DOS is an Attitude Flight Stabilization System (AFSS) and autopilot system.Now can be used for
automated stabilization of fixed wing aircrafts,and after upgrade firmware can be used for other aircraft and
equipment control (For more details of DOS,please refer to the latest firmware and the instructions).
DOS has integrated three-axis gyro ,three-axis accelerometer,three axis magnetometer and barometric
pressure sensor. DOS can accurately measure flight attitude, the earth azimuth and through the barometer to
measure relative altitude. This manual mainly introduces DOS firmware for Multi-rotor flight system.
The firmware for Multi-rotor flight system above V2.20 can realize the following functions:( We will
continue updating new firmware to improve performance and update functions, please pay attention to the
latest news FeiYu official website (www.feiyudz.cn) posted.)
Attitude Stabilized Mode
DOS can auto stabilize the aircraft flight attitude in this mode, pitch and roll stick center position for
0 °attitude,its endpoint is 45 ° , pitch and roll stick can linear control the flight attitude, maximum angular
velocity is 150 ° / s. Yaw stick in the center position will lock current course , its endpoint corresponding
maximum rotation rate 135 ° per second, yaw stick can linear control the aircraft rotation rate. Throttle stick
direct control aircraft climb and decline, climbing and declining rate is directly related to the throttle.
Hovering Mode
The GPS Module must be connected to the DOS with at least 5 GPS satellites detected.In this Mode, yaw
control method is the same as Attitude Stabilized Mode.DOS can auto control flight altitude.Climbing and
descending rate is directly related to the throttle, when the throttle stick is in the center position,DOS auto locks
the altitude, in maximum means climb rate is 3 m/s, in minimum means decline rate is 1.5 m/s.Throttle stick
can linear control the aircraft climb and decline rate.Pitch, roll sticks released will lock the position when GPS
signal is adequate. And non-releasing is stand for the aircraft movement speed in the corresponding axial