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HUBBLEFLY TECHNOLOGIES READY FOR
Hubblefly Starlite
Hubblefly Starlite is an electric, micro, autonomous quadcopter system built specifically to meet the training requirements for unmanned aerial systems. With its full autonomous capability and multiple failsafe features it is safe tool for beginners to advanced users. Starlite is very sturdy in wind conditions upto 8m/s and has very good stability. Highly integrated PCB board simplifies the cabling.
Starlite is integrated with PX4 AUTOPILOT. PX4 is a high-performance autopilot-on-module suitable for multicopter and other robotic platforms that can move.
It is targeted towards high-end research, industrial needs which combine the functionality of the PX4FMU + PX4IO. The Chibios real-time operating system features high performance, flexibility, and reliability for controlling any autonomous vehicle.
Equipment Specifications
Starlite system consists of Air Vehicle, which is the flying component and ground control systems through which it can controlled. Its systems and sub systems are listed below along with their specifications:
| Air Vehicle | MAIN SYSTEM | SUB SYSTEM | PARAMETER | SPECIFICATIONS |
| Airframe (Integrated) | Length | 320 mm | ||
| Width | 320 mm | |||
| Height | 180 mm | |||
| AUW | 1.62 kg | |||
| Number of Rotors | 4 | |||
| Propulsion Type | Electric | |||
| Avionics | Autopilot | Dual Redundant, Integrated AHRS | ||
| Autopilot Firmware | NPNT V1.0 | |||
| GPS | Yes | |||
| Magnetometer | Yes | |||
| Barometer | Yes (with offset correction) | |||
| Power Regulator | Yes (5V) | |||
| Communication | Telemetry Radio | 2.4 GHz | ||
| RC Receiver | 2.4 GHZ | |||
| Propulsion | Motor Type: BLDC | |||
| Battery | Li-Po | |||
| Battery Charger | Input Voltage Range | AC 230V, DC 25 V | ||
Operating Parameters
Basic operating parameters as per standard atmospheric conditions are mentioned below. All performance parameters are measured at sea level at ambient temperature of 25° C.
| Maximum Endurance | 25 Mins |
| Maximum Operating Range | 3 km |
| Altitude Ceiling (AMSL) | 4000 m |
| Operational Limit (AGL) | 200 m |
| Operational Range Limit | 2.5 Km |
| Cruise Velocity | 5 m/s |
| Maximum Operating Temperature | 50° |
| Minimum Operating Temperature | -10° |
| Humidity | 95 RH |
Fail Safe And Safety
| Battery | Yes 30% Warning, 20% Landing, Remotely Adjustable |
| Communication | Yes Loss Warning, Auto Re-establishment, RH on sustained loss |
| Remote Control | Yes Position Hold on loss |
| GeoFence | Yes Enabled RH On Breach |
Hubblefly Starlite
MICRO-QUADCOPTER
AIRFRAME
COMPOSITE BODY
MAX AUM
2 KG
ENDURANCE
20 min
FRAME SIZE
350 MM
NPNT COMPLIANT
FIRMWARE + GCS LICENSE
COMMUNICATION
1 KM
Hubblefly Starlite drone kit contains the following contents:
- Battery
- Ground Radio
- RC Transmitter
- GCS Software License
- Quad Copter with integrated avionics with NPNT capability
Hubblefly Staredge
Hubblefly Staredge is an electric, small, autonomous quadcopter system built specifically to meet the mapping and survey requirements for unmanned aerial systems. With its full autonomous capability and multiple failsafe features it is safe tool for beginners to advanced users.
Staredge quadcopter is a high quality multicopter for professional mapping and survey with high flight performance and heavy loading capacity.
Staredge is sturdy and has very good stability. Crab type landing gear and umbrella-type arm combine to enable a wide range of shooting angles and camera motions. Staredge provides adequate space for switchable payloads.
Staredge is integrated with PX4 AUTOPILOT. PX4 is a high-performance autopilot-on-module suitable for multicopter and other robotic platforms that can move. It is targeted towards high-end research, industrial needs which combine the functionality of the PX4FMU + PX4IO. The Chibios real-time operating system features high performance, flexibility, and reliability for controlling any autonomous vehicle.
Equipment Specifications
Staredge system consists of Air Vehicle, which is the flying component and ground control systems through which it can controlled. Its systems and sub-systems are listed below along with their specifications:
| Air Vehicle | MAIN SYSTEM | SUB SYSTEM | PARAMETER | SPECIFICATIONS |
| Airframe (Integrated) | Length | 500 mm | ||
| Width | 500 mm | |||
| Height | 220 mm | |||
| AUW | 3.4 kg | |||
| Number of Rotors | 4 | |||
| Propulsion Type | Electric | |||
| Avionics | Autopilot | Dual Redundant, Integrated AHRS | ||
| Autopilot Firmware | NPNT V1.0 | |||
| GPS | Yes | |||
| Magnetometer | Yes | |||
| Barometer | Yes (with offset correction) | |||
| Power Regulator | Yes (5V) | |||
| Communication | Telemetry Radio | 2.4 GHz | ||
| RC Receiver | 2.4 GHZ | |||
| Propulsion | Motor Type | BLDC | ||
| Battery | Type | Li-Po | ||
| Battery Charger | Input Voltage Range | AC 230V, DC 25 V | ||
Operating Parameters
Basic operating parameters as per standard atmospheric conditions are mentioned below. All performance parameters are measured at sea level at ambient temperature of 25° C.
| Maximum Endurance | 40 Mins |
| Maximum Operating Range | 5 km |
| Altitude Ceiling (AMSL) | 4000 m |
| Operational Limit (AGL) | 200 m |
| Operational Range Limit | 2.5 Km |
| Cruise Velocity | 5 m/s |
| Maximum Operating Temperature | 50° |
| Minimum Operating Temperature | -10° |
| Humidity | 95 RH |
Fail Safe And Safety
| Battery | Yes 30% Warning, 20% Landing, Remotely Adjustable |
| Communication | Yes Loss Warning, Auto Re-establishment, RH on sustained loss |
| Remote Control | Yes Position Hold on loss |
| Geofence | Yes Enabled RH on breach |
Applications
- 2D orthomosaics
- 3D terrain models & DEMs
- Precision Agriculture
- Power Line Inspection
- Research & Forestry
- Wildlife monitoring
- Oil & gas pipeline
- Geophysical surveys
- Topography
Hubblefly Staredge
SMALL-QUADCOPTER
AIRFRAME
COMPOSITE BODY
MAX AUM
4 KG
ENDURANCE
40 min
FRAME SIZE
500 MM
NPNT COMPLIANT
FIRMWARE + GCS LICENSE
COMMUNICATION
1 KM
Hubblefly Staredge drone kit contains the following contents:
- Battery
- Ground Radio
- RC Transmitter
- GCS Software License
- Quad Copter with integrated avionics with NPNT capability