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Payloads
 

Microview

The Microview is high performance, Electro optical, day/night payload, which its extreme light weight enables to reduce the UAV's size substantially. The Microview is a Gimbaled stabilized reconnaissance payload specially designed for air vehicles in which space and weight are critical issues. The Microview operates during both daytime and nighttime conditions and provides real time video pictures of the target while remotely controlled from the ground control station, via the communication link. The system also provides reports regarding its orientation in space in relation to the UAV axis. The Microview is designed to be installed at the aircraft nose however belly mounting is also possible.
In addition to the Microview, EMIT UAV's are compatible with other manufacturer existing payloads.

 

 
DAY ONLY
DUAL VERSION (DAY/NIGHT)
Visible
IR
type
  • Sony FCB-780BP
  • Sensor: 1/6” type Super HAD CCD 800Kpixels

Electronic image stabilizer (selected under operator’s command)

 

 

 

 

  • Sony FCB-1X10AP
  • Sensor: Ľ” type Super HAD CCD 440Kpixels

 

 

 

 

 

  • OPGAL EYE-25 FLIR
  • VOx Microbolometer
  • 25 ?m pixel size
  • NETD > 35° mK @ 12msec time constant,

50 Hz FR

 

 

 

 

Power consumption
2.7[W]
2.0[W]
<2.2[W]
Type
1/6”
1/4”
384X288
Spectral band
Visible band
Visible band
8-12[µm]
50 Hz
50 Hz
50 Hz

Video output

PAL
PAL
PAL

 

 
DAY ONLY
DUAL VERSION (DAY/NIGHT)
Visible
IR
Optics
  • 60 [mm] Zoom Lens
X 25 Optical

 

    • 40 [mm] Zoom Lens
    • X 10 Optical

     

Focal length 50[mm]

f/0.8 Germanium lens

Filed of View
Narrow
1.1?
4.6?
2.5? (Digital)
Wide
21?
45?
10?
Sensitivity
Minimum  Illumination: 2.5 [lux]
Minimum  Illumination: 2.0 [lux]
Thermal sensitivity:< 0.050°C
Target detection (Small vehicle size 5 X 2.5m)
12 [Km]
8[Km]
2.5 [Km]
Target recognition
5 [Km]
3.5 [Km]
1.5 [Km]
Sensor weight
350 [g]
95 [g]
5 1 0 [g]
Tracker Mode
Correlative, Centroid, Area

Main mechanical characteristics

 
DAY ONLY
DUAL VERSION (DAY/NIGHT)
Visible
IR
Diameter
170    [mm]
Length
335    [mm]
Weight
7 [Kg] INCLUDE ALL ELECTRONICS
Four Gimbals System

Hierarchical Structure:

Primary: Pitch-Roll axis
Secondary:          Pitch-Yaw axis

Electro Mechanical specifications

Field of Regard
Roll- axis       ± 140?
Optional            360?
Pitch- axis
Day Only
Day/Night
-135.5? to  + 40?
-110.0? to  + 40?
Slew rate
Angular acceleration
0-1[Rad/sec]
0-1[Rad/sec2]
Relative Excursion angle between
Outer and Inner systems
Pitch axis
3.5?
Yaw
6.0?
Stabilization
better than   25 [µrad] RMS on axis

Electrical interface

Power requirement
24[V],   max  60 [w]
Communication
RS-422,RS232

Environmental conditions

 
DAY ONLY
DUAL VERSION (DAY/NIGHT)
Visible
IR
Flight speed
up to - 250  [Knots]
Max Operational Altitude
25,000 [ft]
Temperature
Operational
-30[?C] to + 55[?C]
Storage
-40[?C] to + 80[?C]
Humidity
Up to 95% non condensing
Water tightness (pressure gauge)
1[psi]
Vibration level
1.3 [gRms]
Shock Level
X axis  20 [g] for 6 [msec]
Linear acceleration:
Pitch  10[g] for 6 [msec]
Yaw  10[g] for 6 [msec]

 

 

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