Strong ally for long distance flight.
GNAS SKY’s single-rotor helicopter capable of freely flying about the sky like a real helicopter.
Complete missions with certainty even under poor conditions such as strong wind at sea
and frequent turbulence in mountainous area.
Complete missions with certainty even under poor conditions such as strong wind at sea
and frequent turbulence in mountainous area.
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POINT1All products are domestically produced original
Equipped with “GNAS SKY CORE” & High-performance motion sensor, 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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POINT3Resistant to wind.
With its overwhelming strength achieved against strong and gusty wind compared with conventional drone, it will never get unstable even during descending. Capable of stable flight even under a wind speed exceeding 15 m/s.
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POINT4A wide variety of options.
Mounted GNAS SKY CORE automatically detects even unexpected obstacles. Achieve stable flight while reducing collision damage during automatic flight.
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POINT5Get to the site fast.
It can cruise at up to 72 km/h. Arrive at the scene as soon as possible and complete your mission.
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POINT6Pilot 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 SINGLE ROTOR HELICOPTER
| Specification | Note | ||
|---|---|---|---|
| Airframe | Aircraft Type | Single-Rotor Helicopter | |
| Max Length | 2,070mm | Include Rotor | |
| Body Length | 1,500mm | Without Rotor | |
| Width | 380mm | ||
| Hight | 400mm | ||
| Rotor Diameter | 900mm | ||
| Weight | Aircraft Weight | Less than 8kg | Without Battery |
| Battery Weight | Less than 4kg | ||
| 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 | 17,000mAh/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 | 25m/s | |
| Max Lifting Speed | 5m/s | ||
| Max Dropping Speed | 3m/s | ||
| Maximum altitude (theoretical) |
Height 3,000m | There is a legal limit of altitude above 150m | |
| Wind Resistance | 20m/s | Flight performance at around 5m/s is retained at the time of its maximum takeoff weight. | |
| Max Aungular Rate | More than 3rad/s | Non-Payload Operation | |
| Hovering position performance |
Horizontal position： Less than ±1m |
Windless conditions, GNSS reception status | |
| 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. 40min. | |
| 3kg Payload Operation | 23min. | ||
| 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. | |
