substances and incomplete assembly, main components with obvious
failures, spare parts with obvious defect or missing), but still use the
equipment and cause damages.
5. Any damage caused by flying the drone in magnetic interference zone, radio
interference zone, no-fly zone, or the pilot flies the drone with following
conditions such as in a shadow, poor light, blurred vision and vision
obscured.
6. Collision, overturns and force majeure as fire, storms, tornadoes, heavy
rains, floods, tsunamis, earthquakes etc.
7. Direct or indirect liability for any illegal use, or other unauthorized purposes.
8. Third-party liability arising from the use of our software and hardware
products .
9. Any loss caused by obtaining or using our software or hardware and related
manuals through unauthorized ways.
10. Other losses that are not within the AheadX’s sphere of accountability.
Introduction
LEO GNC (Micro Guidance Navigation Control System) is a new generation of
navigation flight control system designed for industrial-grade drones. It features
with high integration, high reliability and high cost performance. It supports VTOL
quad plane, fixed wing, helicopter, multi-rotor and other types of aircraft. .
LEO integrates IMU and a datalink with max 60km communication distance into
the control system. It equips with -15℃～85℃ temperature compensation MES
sensor and J30 aviation connector. LEO adopts a decoupled extended Kalman
filter, improved L1 guidance rate, and ADRC controller as core algorithm, which
has extremely high precision.
Features and applications
MEMS inertial measurement unit, triaxial magnetometer, barometric altimeter,
airspeed meter, GNSS module, triaxial magnetometer, barometric altimeter,
air speedometer, GNSS module. -15~85℃ temperature compensation for
MEMS IMU and triaxial magnetometer.
Built-in 900MHz data link, communication distance up to 60km*.
Dual integrated navigation system. Decoupled 17-order extended Kalman
filter to complete the information fusion. Automatically switch between the
GNSS/INS and AHRS/DR navigation modes according to satellite signals
Built-in shock absorption structure to reduce the impact caused by vibration
to IMU
Iproved L1 guidance rate and ADRC controller to improve control accuracy
and robustness.
With built-in global geomagnetic model, and compass calibration has been
tested in polar area. LEO can complete one-key compass calibration, take off
immediately after satellite positioning.
