Specification | Note | ||
---|---|---|---|
Airframe | Aircraft Type | Quad Multicopter Type | |
Diagonal Length | 1950mm | Include Rotor | |
Length | 840mm | Without Rotor | |
Width | 840mm (Ready to fly) | ||
400mm (Folding) | |||
Hight | 480mm (Ready to fly) | ||
300mm (Folding) | |||
Rotor Diameter | 760mm | ||
Weight | Aircraft Weight | Less than 6kg | Without Battery |
Battery Weight | Less than 5.3kg | ||
Battery capacity | Mail Battery | 22,000mAh/44.4V | LiPo Battery, 12cells |
Flight Control System |
Motion Sensor | CSM-MG200 | In-house development |
Flight Controller | GNAS SKY TYPE-S Series | In-house development | |
Radio Control Module (selectable) |
2.4GHz | 300 m (line-of-sight distance) Transmitter of FUTABA |
|
169MHz(1W) | More than 5km Line of sight distance Radio License Required |
||
Telemetry Radio Module (selectable) |
2.4GHz | Max 500m Line of sight distance |
|
2.4GHz(1W) | More than 5km Line of sight distance Radio License Required |
||
Buffer Puck | 5,000mAh/11.1V | LiPo Battery, 3cells(share the payload power supply) | |
Enviroment Resistance |
Operating Temperature | 0℃~+50℃ | |
Humidity | Less than 98% | without condensation | |
Water-proof performance | IPx3 |
Performance | Note | ||
---|---|---|---|
Flight Performance |
Max Cruise Speed | 20m/s | |
Max Lifting Speed | 5m/s | ||
Max Dropping Speed | 3m/s | ||
Wind Resistance | MAX 18m/s | Flight performance at around 2 m/s is retained at the time of its maximum takeoff weight. | |
Max Aungular Rate | More than 2rad/s | Non-Payload Operation | |
Max thrust | More than 300N | ||
Maximum takeoff weight | Max takeoff Weight | 15kg | Payload of 3 kg is assumed. (*Negotiable for mounting of payload exceeding 3 kg.) |
Flight time (hovering) |
Non-Payload Operaton | Max. 45min. | |
3kg Payload Operation | 30min. |
Flight function | ||
---|---|---|
Flight mode (3-mode selection switching) |
Angular velocity control mode | A flight mode to maintain tilt of the airframe (not to restore level state) |
Attitude control mode | A flight mode to maintain only level state of the airframe | |
GNSS assist mode | A flight mode to keep level position | |
Flight state selection (ON/OFF) |
Available to select Altitude control | Altitude control OFF/Ground altitude maintenance/GNSS altitude maintenance Operable during attitude controlling and GNSS-assisted controlling. |
Auto pilot | Automated flight is carried out. Available only during GNSS-assisted mode. | |
RTH | Automatically return to home position. Available only during GNSS-assisted mode. |