GNAS SKY
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.
  • POINT1

    All 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!
    All products are domestically produced original
  • POINT2

    Programmed automatic flight.

    Programmed automatic flight is available by GNAS SKY CORE flight control program. Flight just as you imagined is achieved by diverse settings.
    Programmed automatic flight
  • POINT3

    Outstanding 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.
    Resistant to wind
QUAD MULTICOPTER
  • POINT4

    Sufficient 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.
    Secured obstacle detection capability
  • POINT5

    Secured 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.
    Secured obstacle detection capability

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.
Flight time and payload