INDELA-SKY.SPIDER
Remote monitoring complex based on a vertical takeoff and landing unmanned aerial vehicle and a ground control and information processing station
Description
Remote monitoring complex with unmanned aerial vehicles «INDELA-SKY.SPIDER» is a complex that ensures real-time reception of information from a gyro-stabilized optoelectronic system at a
distance of up to 15 km within line of sight from a ground control station.
Ground control station (NSU) as ground equipment includes all the necessary components for flight programmed control and prompt equipment diagnostics. The «INDELA-SKY.SPIDER»
is designed:
- to deliver useful load equipment to a selected place;
- to assure its functioning on command from a ground control station or from an on-board computer;
- real-time visual data transmission to a ground control station or from on-board storage devices;
Characteristics
| Engine | commutatorless motor | |
| Statistical traction | N | 108 |
| Key geometric characteristics | ||
| Length with main rotor | mm | 1580 |
| Height | mm | 434 |
| Wheelbase | mm | 1020 |
| Weight data | ||
| Weight | kg | 7,2 |
| Basic flight characteristics | ||
| Cruise speed | km/h | 40 |
| Flight duration (depends on the temperature and wind speed) | minute | from 20 to 40 |
| Wind (takeoff and landing) | m/s | up to 12 |
| Operating temperature | C | -15 … +55 |
UAV useful load components
Biaxial gyro-stabilized suspension «INDELA OGD-20HIR» ensures high level of stabilization due to the up-to-date gyroscopes of the leading manufacturers and modern software.
«INDELA-SKY.SPIDER» carrier with a gyro-stabilized optoelectronic system «INDELA OGD-20HIR» with an infrared camera
Complex includes:
«INDELA-SKY.SPIDER» carrier with a gyro-stabilized optoelectronic system «INDELA OGD-20HIR» with an infrared camera
«INDELA-GC» ground control station
Characteristics
| Indela OG-20HIR’s characteristics | ||
| Resolution | 1920х1080 | |
| Quantity of active pixels | 2 000 000 | |
| Image sensor | 1/3 –type CMOS | |
| Signal system | HD:1080p/29.97, 1080i/59.94 SD:NTSC/PAL | |
| Lens | f = 4.7 mm (wide), 94 mm(tele) F 1.6 (wide), F 3.5 (tele) | |
| Optical magnification, not less than | 20x | |
| Digital magnification | 10х (200 with optical) | |
| Viewing angle | 54.1°(wide), 2.9°(wide) | |
| Minimum object distance | 10 mm (wide), 1000 mm (tele) | |
| Synchronizing system | internal | |
| Camera sensitivity, not less than | 1,7 Lux | |
| Signal/noise ratio | more than 50dB | |
| Electronic shutter | from 1/2 to 1/10 000 s, 21 steps | |
| White balance | Auto, ATW, manual, indoors, outdoors, outside a car, «one-push», sodium lamp (fixed/auto) | |
| Intensification | Auto/Manual/Max(from -3 dB to 28dB, 2 steps) | |
| Background light compensation | Yes | |
| Focusing system | Automatic/Manual | |
| Digital video output | HD:Y/Cb/Cr 4:2:2 EIA/CEA-861-B type via LVDS(Y:8 bit, C: 8 bit, Vsync, Hsync, Field, Clock) | |
| Analog video output | HD: Component(Y/Pb/Pr) SD: VBS | |
| Compression | Yes | |
| Improved noise clipping | Yes | |
| Blink suppression | Auto | |
| Automatic stabilization of camera’s optical axis at a set direction in the geocentric coordinate system, being at rest, with accuracy, not worse than | 1,5° | |
| High-resolution infrared camera | ||
| System type | Uncooled | |
| Sensor type | infrared thermal image converter , 640 x 512 VOx Microbolometer | |
| Pixel size | 25 μm | |
| Spectral range | 7.5 – 13.5 μm | |
| Operational characteristics | < 65mK NEdT при f/1.0 | |
| Image inversion and return | 2х and 4х digital zoom | |
| Digital image enhancement | ||
| Power dissipation (statistic) | less than 3 watt | |
| Readiness for image transmission | less than 4 s | |
| Bonding technique | Under the aircraft | |
| General system or airspace operation | RS-485 Ethernet | |
| Identification of the object selected by the operator | Yes (limited) | |
| Tracking the object selected by the operator | Yes | |
| Adjustable OSD | Yes | |
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