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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POINT3High safety and energy saving effect.
The use of a variable pitch mechanism for propeller control leads to the recovery and stabilization of flight attitude at an overwhelmingly fast rate compared to fixed pitch aircraft. In addition, since the propeller speed can be kept constant, energy-saving flight is possible, contributing greatly to the realization of safe, long-distance flight.
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POINT4Sufficient payload capacity.
Even though it is an electric type, it can fly for more than 30 minutes with a payload of 3kg. Long flight time is possible even 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.
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POINT6Wide variety of options.
Achieved for more than 30 minutes of flight with a load capacity of 3 kg even by electrically-powered type. Capable of loading 6 kg of weight with an optional 29-inch propeller! In addition to high-performance digital and infrared cameras, it is capable of mounting payloads such as daily necessaries and medical products in accordance with their usage.
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POINT7Pilot assisting function.
Based on information of a ground altitude sensor mounted on the body, it improves safety of flight by supporting the pilot in various situations.
・Speed control at a low altitude
・Minimum altitude holding function*
*This function can be kept OFF.
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 | ||
| 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 |
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| 169MHz(1W) | More than 5km Line of sight distance Radio License Required |
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| Telemetry Radio Module (selectable) |
2.4GHz | Max 500m Line of sight distance |
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| 2.4GHz(1W) | More than 5km Line of sight distance Radio License Required |
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| 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. | |
