Overwhelming stability
Proved technology and reliability It is achieved precisely because of industrial UAV.
GNAS SKY Quad Multicopter embodied by fusion of a mechanism and control technology
led by aviation professionals.
With its overwhelming stability, remarkably useful in various situations and for use applications.
GNAS SKY Quad Multicopter embodied by fusion of a mechanism and control technology
led by aviation professionals.
With its overwhelming stability, remarkably useful in various situations and for use applications.
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POINT1All products are domestically produced original
Equipped with “GNAS SKY CORE” & High-performance motion sensor CSM-MG200, our original flight control program developed by mobilizing all available in-house resources. All products from airframe to flight control, communication and flight support systems are based on domestic integrated manufacturing!
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POINT2Programmed automatic flight.
Programmed automatic flight is available by GNAS SKY CORE flight control program. Flight just as you imagined is achieved by diverse settings.
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POINT3Outstanding stability
Adopted controllable-pitch mechanism for propeller control. Achieved overwhelming robustness against strong and gusting wind compared with conventional drones, causing no unstable state even during descending.
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POINT4Sufficient payload capacity
Realized more than 30 minutes of flight even with a payload of 3 kg. Long flight is possible even loading with heavy equipment.
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POINT5Secured obstacle detection capability.
Unexpected obstacle is automatically detected by an obstacle sensor mounted on the front part. Achieve stable flight while reducing collision damage during automatic flight.
GNAS SKY QUAD MULTICOPTER
| 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 | ||
| Flight Control System |
Motion Sensor | CSM-MG200 | In-house development |
| Flight Controller | GNAS SKY TYPE-S2 | 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 |
||
| Battery | Mail Battery | 22,000mAh/44.4V | LiPo Battery, 12cells |
| 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. | ||
| Fight 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 airfame | |
| 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. | |
