Owner's Manual
Table Of Contents
- User Manual
- Quick Start Guide
- Multi-channel Charger Guidelines
- Battery Safe Operation Guidelines
- Disclaimer and Safety Operation Guidelines
2. Ludicrous mode
Use the GPS module and downward vision system to realize accurate hovering. After the
aircraft control sensibility is adjusted, the maximum flight speed will rise to 15m/s, the
maximum rising speed will be 5m/s, and the maximum descending speed will be 4m/s.
3. Smooth mode
Limit the flight speed based on standard mode, namely, the maximum flight speed as 5m/s,
the maximum rising speed as 3m/s and the maximum descending speed as 2m/s, to make the
aircraft more stable during shooting.
The aircraft will enter the attitude (ATTI) mode when the GPS signal is poor, the compass is
disturbed and the vision positioning conditions fail to be met. Under the ATTI mode, the
aircraft will drift horizontally, and the intelligent flight function and the return function will
not be available. Therefore, the aircraft under this mode cannot realize spot hover and
automatic brake, so it shall be landed on a safe position as soon as possible to avoid the
occurrence of accident. User shall try to avoid the flight in poor GPS signal, non-ideal light
condition and narrow space, in order to avoid the flight accident due to the ATTI mode.
Important
In the case of flight under the ludicrous mode, the flight speed of the aircraft will
increase largely compared with the normal mode, thus resulting in the substantial
increase in braking distance. In the case of flight without wind, user shall reserve at least
30m of braking distance to ensure flight safety.
In the case of flight under the ludicrous mode, the descending speed of the aircraft will
also increase largely; in the case of flight without wind, user shall reserve at least 10m of
braking distance to ensure flight safety.
In the case of flight under the ludicrous mode, the attitude control sensibility of the
aircraft will increase largely compared with the normal mode. Specifically, any operation
in a small extent on the remote controller will cause a substantial flight action of the
aircraft. In the actual flight, user shall reserve the enough flight space to ensure flight
safety.
After starting shooting under the standard mode or the smooth mode, in order to ensure
the shooting stability, the flight speed will be limited when the gimbal pitch angle is
close to -90° or 0°. In the case of high wind, the limitation will be relieved to improve
the wind resistance of the aircraft. At this time, the gimbal shake may occur.