• Range of measured angular rate, deg/sec: ±40
• Bias drift at fixed temperature deg/h: <0.005
• Bias drift at changing temperature from -30°C to 50°C, deg/h: <0.05
• Scale factor repeatability, %: <0.01
• Bandwidth, Hz: >50
• Random walk, deg/√h: <0.0005
• Power supply: 5V±0.25*
• Power consumption, W: <7
• Weight (net), kg: 1.7
• Dimensions, mm: Ø250×4
• Output: RS485**

 
* Optional: from 18 to 36V
** Optional – RS232/RS422, Discrete – Unitary Code (Frequency is proportional to measured angular rate)
 
The export of SRS2000 gyros is under strict government control due to its precision characteristics. Export license is granted upon the International Import Certificate (End Use Certificate) issued by the authorized Ministry of the end user’s country and the end use certificate issued by the ultimate end user reflecting the detailed intended civil end use of the Goods. Besides that, the end user company undertakes to grant the right to inspect the Goods supplied at any time. Please allow 2-3 months for the process; positive outcome is not guaranteed even in case all the required documents are presented.

• Range of measured angular rate, deg/sec: ±40
• Bias drift at fixed temperature deg/h: ≤0.007
• Bias drift at changing temperature from -30°C to 50°C, deg/h: ≤0.05
• Scale factor repeatability, %: ≤0.02
• Bandwidth, Hz: >50
• Random walk, deg/√h: <0.0007
• Power supply: 5V±0.25
• Power consumption, W: <7
• Weight (net), kg: 0.9
• Dimensions, mm: Ø150×45
• Output: RS485

 
 
 
The export of SRS1000 gyros is under strict government control due to its precision characteristics. Export license is granted upon the International Import Certificate (End Use Certificate) issued by the authorized Ministry of the end user’s country and the end use certificate issued by the ultimate end user reflecting the detailed intended civil end use of the Goods. Besides that, the end user company undertakes to grant the right to inspect the Goods supplied at any time. Please allow 2-3 months for the process; positive outcome is not guaranteed even in case all the required documents are presented.

• Range of measured angular rate, deg/sec: ±90
• Bias drift at fixed temperature deg/h: <0.02
• Bias drift at changing temperature from -30°C to 50°C, deg/h: <0.1
• Scale factor repeatability, %: <0.05
• Bandwidth, Hz: >50
• Random walk, deg/√h: <0.0002
• Power supply: 5V±0.25
• Power consumption, W: <7
• Weight (net), kg: 0.9
• Dimensions, mm: Ø150×45
• Output: RS485

 
 
 
The export of SRS1000 gyros is under strict government control due to its precision characteristics. Export license is granted upon the International Import Certificate (End Use Certificate) issued by the authorized Ministry of the end user’s country and the end use certificate issued by the ultimate end user reflecting the detailed intended civil end use of the Goods. Besides that, the end user company undertakes to grant the right to inspect the Goods supplied at any time. Please allow 2-3 months for the process; positive outcome is not guaranteed even in case all the required documents are presented.

• Range of measured angular rate, deg/sec: ±1000
• Bias drift at fixed temperature deg/h: ≤0.007
• Bias drift at changing temperature from -30°C to 50°C, deg/h: ≤0.05
• Scale factor repeatability, ppm: ≤100
• Bandwidth, Hz: >50
• Random walk, deg/√h: ≤0.0007
• Power supply: 5V±0.25
• Power consumption, W: <7
• Weight (net), kg: 0.9
• Dimensions, mm: Ø150×45
• Output: RS485

 
The export of SRS1001 gyros is under strict government control due to its precision characteristics. Export license is granted upon the International Import Certificate (End Use Certificate) issued by the authorized Ministry of the end user’s country and the end use certificate issued by the ultimate end user reflecting the detailed intended civil end use of the Goods. Besides that, the end user company undertakes to grant the right to inspect the Goods supplied at any time. Please allow 2-3 months for the process; positive outcome is not guaranteed even in case all the required documents are presented.

• Range of measured angular rate, deg/sec: ±250
• Bias drift at fixed temperature deg/h: ≤0.03
• Bias drift at changing temperature from -30°C to +50°C, deg/h: <0.2
• Scale factor repeatability, %: <0.05
• Bandwidth, Hz: >100
• Random walk, deg/√h: <0.005
• Power supply: 5V±0.25
• Power consumption, W: <7
• Weight (net), kg: 0.35
• Dimensions, mm: Ø100×30
• Output: RS485

• Range of measured angular rate, deg/sec: ±750
• Bias drift at fixed temperature deg/h: ≤0.5
• Bias drift at changing temperature from -30°C to 50°C, deg/h: <1.0
• Scale factor repeatability, ppm: <0.1
• Bandwidth, Hz: >500
• Random walk, deg/√h: <0.01
• Power supply: 5V±0.25*
• Power consumption, W: <6
• Weight (net), kg: 0.2
• Dimensions, mm: Ø70×28
• Output: RS485 or RS422

 
* Optional: from 18 to 36V

• Range of measured angular rate, deg/sec: ±300
• Bias drift at fixed temperature deg/h: ≤0.1
• Bias drift at changing temperature from -30°C to +50°C, deg/h: ≤0.5
• Scale factor repeatability, %: <0.08
• Bandwidth, Hz: >100
• Random walk, deg/√h: <0.007
• Power supply: 5V±0.25*
• Power consumption, W: <8
• Weight (net), kg: 1.2
• Dimensions, mm: Ø110x110x92
• Output: RS485**

 
* Optional: from 18 to 36V
** Optional – RS232/RS422, Discrete – Unitary Code (Frequency is proportional to measured angular rate)

• Range of measured angular rate, deg/sec: ±300
• Bias drift at fixed temperature deg/h: ≤0.5
• Bias drift at changing temperature from -30°C to 50°C, deg/h: ≤1.5
• Scale factor repeatability, ppm: <0.1
• Bandwidth, Hz: >100
• Random walk, deg/√h: <0.01
• Power supply: 5V±0.25*
• Power consumption, W: <8
• Weight (net), kg: 1.2
• Dimensions, mm: 110x110x92
• Output: RS485**

 
* Optional: from 18 to 36V
** Optional – RS232/RS422, Discrete – Unitary Code (Frequency is proportional to measured angular rate)

Gyro (TFOS-500)

• Angular rate range: ±300 deg/sec
• Bias repeatability on operation temperature: <0.1 deg/hr
• Scale factor repeatability: 0.008 % (RMS)
• Random walk: 0.007 deg/√h

 
Accelerometer (AT-1104)

• Range: ±40 g
• Bias repeatability: <1 mg
• Noise: <70 μg (RMS)

 
Physical Characteristics

• Misalignment: <1.5 mrad
• Output sample rate: up to 1000 Hz
• Power supply: 5 VDC or 24 ~ 36 VDC
• Digital output interface: RS 485 or RS422
• Operation temperature: -30°C ~ +60°C
• Storage temperature: -40°C ~ +80°C
• Dimensions: 110 x 110 x 90 mm
• Weight: 1.4 kg

Gyro (TFOS-500)

• Angular rate range: ±300 deg/sec
• Bias repeatability on operation temperature: <0.5 deg/hr
• Scale factor repeatability: 0.05% (RMS)
• Random walk: 0.01 deg/√h

Accelerometer (AT-1104)

• Range: ±35 g
• Bias repeatability: <1 mg
• Noise: <70 μg (RMS)

Physical Characteristics

• Misalignment: <1.5 mrad
• Output sample rate: up to 1000 Hz
• Power supply: 5 VDC or 24 ~ 36 VDC
• Digital output interface: RS 485 or RS422
• Operation temperature: -30°C ~ +60°C
• Storage temperature: -40°C ~ +80°C
• Dimensions: 110 x 110 x 90 mm
• Weight: 1.4 kg

Gyroscopes (SFOS1000)

• Angular rate range: ±90 deg/sec
• Bias drift on stabilized temperature: <0.01 deg/hr (RMS)
• Bias drift in temperature range -40°C ~ +60°C: <0.1 deg/hr (RMS)
• Bias repeatability on stabilized temperature: <0.01 deg/hr (RMS)
• Scale factor error: <0.005% (RMS)
• Random walk: <0.0005 deg/√h (RMS)
• Bandwidth: >100 Hz

 
Accelerometers

• Range: ±10…±50 g
• Bias drift on stabilized temperature: <0.05 mg (RMS)
• Bias drift in temperature range -40°C ~+60°C: <0.5 mg (RMS)
• Bias repeatability on stabilized temperature: <0.08 mg (RMS)
• Scale factor error: <0.05% (RMS)
• Random walk: <0.04 mg/√Hz (RMS)
• Bandwidth: >100 Hz

 
Physical Characteristics

• Misalignment: <5 arc.min
• Misalignment stability: <2 arc.min
• Power supply: 27 VDC or 5 VDC
• Digital output interface: RS422 or RS485
• Operation temperature: -40°C ~ +60°C
• Dimensions: 215x 217 x 175mm
• Weight: 5kg

 
 
The export of IFOS1000 is under strict government control due to its precision characteristics. Export license is granted upon the International Import Certificate (End Use Certificate) issued by the authorized Ministry of the end user’s country and the end use certificate issued by the ultimate end user reflecting the detailed intended civil end use of the Goods. Besides that, the end user company undertakes to grant the right to inspect the Goods supplied at any time. Please allow 2-3 months for the process; positive outcome is not guaranteed even in case all the required documents are presented.

Gyroscopes (SFOS501)

• Angular rate range: ±250 deg/sec
• Bias drift on stabilized temperature: < 0.03 deg/hr (RMS)
• Bias drift in temperature range -40°C ~ +60°C: <0.2 deg/hr (RMS
• Scale factor error: 0,05%
• Random walk: <0.005 deg/√h (RMS)
• Bandwidth: >100 Hz

 
Accelerometers

• Range: ±40 g
• Bias drift on stabilized temperature: < 0.05 mg (RMS)
• Bias drift in temperature range -40°C ~+60°C: < 0.5 mg (RMS)
• Bias repeatability on stabilized temperature: < 0.08 mg (RMS)
• Scale factor error: 0,05%
• Random walk: < 0.04 mg/√Hz (RMS)
• Bandwidth: >100 Hz

 
Physical Characteristics

• Misalignment: <5 arc.min
• Misalignment stability: <2 arc.min
• Power supply: 27 VDC or 5 VDC
• Digital output interface: RS422 or RS485
• Operation temperature: -40°C ~ +60°C
• Dimensions: 155 x 140 x 110mm
• Weight: 3kg

 
 
The export of IFOS501 is under strict government control due to its precision characteristics. Export license is granted upon the International Import Certificate (End Use Certificate) issued by the authorized Ministry of the end user’s country and the end use certificate issued by the ultimate end user reflecting the detailed intended civil end use of the Goods. Besides that, the end user company undertakes to grant the right to inspect the Goods supplied at any time. Please allow 2-3 months for the process; positive outcome is not guaranteed even in case all the required documents are presented.

Pure SINS performance (inertial mode)

•        Position accuracy: 20km
•        Velocity accuracy: 14 km/h
•        Heading accuracy: 0.5*sec(lat)°°
•        Pitch and roll accuracy: 0.3°

 
GPS-GLONASS/SINS performance

•        Position accuracy: 20m
•        Velocity accuracy: 0.1m/sec

• Initialization time: 10 min
• Gyro bias drift (1s): ≤0.1°/h
• Accelerometer bias drift (1s): ≤5×10-5g
• Interfaces: MIL-STD-1553B, RS-422/485
• Power supply: 27 V DC
• Power consumption: 14 W
• Size: 240x160x110mm
• Weight: 3.4 kg

 
Operating ranges

•        Angular rate: ≤300 °/sec
•        Linear accelerations: to 10g
•        Vibration: to 2000 Hz
•        Thermal operating range: -40 °C to +60 °C

Pure SINS performance (inertial mode)

•        Position accuracy: 7km
•        Velocity accuracy: 8km/h
•        Heading accuracy: 0.4*sec(lat)°°
•        Pitch and roll accuracy: 0.3°

 
GPS-GLONASS/SINS performance

•        Position accuracy: 20m
•        Velocity accuracy: 0.1m/sec

• Initialization time: 10min
• Gyro bias drift (1s): ≤0.1°/h
• Accelerometer bias drift (1s): ≤10-4g
• Interfaces: MIL-STD-1553B, RS-422/485
• Power supply: 27V DC
• Power consumption: 20W
• Size: 343x185x120mm
• Weight: 6.4kg

•       Range of measured angular rate, deg/sec: ±12 (±550 possible)
•       Bias drift at fixed temperature deg/h:
  ≤0.001 (RMS with 100 second averaging)
  ≤0.00008 (Alan variance)
•       Scale factor repeatability, ppm: 50
•       Bandwidth, Hz: >50
•       Random walk, deg/√h:
  <0.0001 (RMS with 100 second averaging)
  <0.00007 (Alan variance)

•       Power supply: 5V±0.25
•       Power consumption, W: <7
•       Weight (net), kg: 1.7
•       Dimensions, mm: Ø250×45
•       Interfaces: RS485

The export of SFOS-5000 is under strict government control due to its precision characteristics. Export license is granted upon the International Import Certificate (End Use Certificate) issued by the authorized Ministry of the end user’s country and the end use certificate issued by the ultimate end user reflecting the detailed intended civil end use of the Goods. Besides that, the end user company undertakes to grant the right to inspect the Goods supplied at any time. Please allow 2-3 months for the process; positive outcome is not guaranteed even in case all the required documents are presented.

• Range of measured angular rate, deg/sec: ±30
• Bias drift at fixed temperature deg/h:
  ≤0.03 (RMS with 100 second averaging)
  ≤ 0.0012 (Alan variance)
• Bias drift at changing temperature from -30°C to +40°C, deg/h:
  <0.07(RMS)
• Scale factor repeatability, ppm: <500
• Bandwidth, Hz: >100
• Random walk, deg/√h:
  <0.005 (RMS with 100 second averaging)
  <0.0025 (Alan variance)
• Power supply, V: 27
• Power consumption, W: <20
• Weight (net), kg: 2.6
• Dimensions, mm: 172 x 176 x 110
• Output: 1553 MIL STD

Pure SINS performance (inertial mode, RMS)

•        Position accuracy: 4km
•        Velocity accuracy: 1km/h
•        Heading accuracy: <0.1*sec(lat)°°
•        Pitch and roll accuracy: <0.05°

 
GPS-GLONASS/SINS performance (RMS)

•        Position accuracy: 20m
•        Velocity accuracy: 0.1m/sec

• Initialization time: 10min
• Gyro bias drift (1s): ≤0.03°/h
• Accelerometer bias drift (1s): ≤1×10-4g
• Interfaces: MIL-STD-1553B or RS-422/485
• Power supply: 27V DC
• Power consumption: 20W
• Size: 286x163x124 mm
• Weight: 4.8 kg

 
Operating ranges

•        Angular rate: ≤250°/sec
•        Linear accelerations: to 10g
•        Vibration: to 2000 Hz
•        Thermal operating range: -40 °C to +60 °C

Pure SINS performance (inertial mode, RMS)

•        Position accuracy: 1.6km
•        Velocity accuracy: 0.04km/h
•        Heading accuracy: <0.03*sec(lat)°°
•        Pitch and roll accuracy: <0.02°

 
GPS-GLONASS/SINS performance (RMS)

•        Position accuracy: 20m
•        Velocity accuracy: 0.1m/sec

• Initialization time: 10min
• Gyro bias drift (1s): ≤0.01°/h
• Accelerometer bias drift (1s): ≤1×10–5g
• Interfaces: MIL-STD-1553B or RS-422/485
• Power supply: 27V DC
• Power consumption: 20W
• Size: 171x224x252mm
• Weight: 6.4 kg

 
Operating ranges

•        Angular rate: ≤100°/sec
•        Linear accelerations: to 10g
•        Vibration: to 2000 Hz
•        Thermal operating range: -40 °C to +60 °C

Gyro (TFOS-500)

• Angular rate range: ±300 deg/sec
• Bias repeatability on operation temperature: < 0.1 deg/hr
• Scale factor repeatability, ppm: 500 (RMS)
• Random walk: 0.007 deg/√h

Accelerometer

• Range: ±10 g to ±40 g
• Bias repeatability: < 1 mg
• Noise: < 70 μg (RMS)

Physical Characteristics

• Misalignment: < 1.5 mrad
• Output sample rate: up to 1000 Hz
• Power supply: 5 VDC or 24 ~ 36 VDC
• Digital output interface: RS 485 or RS422
• Operation temperature:-30°C ~ +60°C
• Storage temperature: -40°C ~ +80°C
• Dimensions:110 x 110 x 90 mm
• Weight: 2.4 kg

Gyroscopes (SFOS-501)

• Angular rate range: ±300 deg/sec
  (±1000 deg/sec is possible)
• Bias drift on stabilized temperature: < 0.03 deg/hr (RMS)
• Bias drift in temperature range -40°C ~ +60°C: <0.2 deg/hr (RMS)
• Scale factor error, ppm: 300 (RMS)
• Random walk: <0.005 deg/√h (RMS)
• Bandwidth: >100 Hz

Accelerometers

• Range: ±10 to ±40 g
• Bias drift on stabilized temperature: < 0.05 mg (RMS)
• Bias drift in temperature range -40°C ~+60°C: < 0.5 mg (RMS)
• Bias repeatability on stabilized temperature: < 0.08 mg (RMS)
• Scale factor error: <0.05% (RMS)
• Random walk: < 0.04 mg/√Hz (RMS)
• Bandwidth: >100 Hz

Physical Characteristics

• Misalignment: <5 arc.min
• Misalignment stability: <2 arc.min
• Power supply: 20 -36 VDC
• Digital output interface: RS422 or RS485
• Operation temperature: -40°C ~ +60°C
• Dimensions: 142 x 280 mm
• Weight: 6 kg

Gyro (TFOS-1000)

• Angular rate range: ±550 deg/sec
• Bias drift on stabilized temperature:   < 0.01 deg/hr (RMS)
• Bias drift in temperature range -40°C ~ +60°C:    < 0.1 deg/hr (RMS)
• Bias repeatability on stabilized temperature:    < 0.01 deg/hr (RMS)
• Scale factor error, ppm:   100 (RMS)
• Random walk:   <0.0005 deg/√h (RMS)
• Bandwidth:   >100 Hz

Accelerometers

• Range: ±10 g to ±50 g
• Bias drift on stabilized temperature:   < 0.05 mg (RMS)
• Bias drift in temperature range -40°C ~+60°C:   < 0.5 mg (RMS)
• Bias repeatability on stabilized temperature:   < 0.08 mg (RMS)
• Scale factor error:   <0.05% (RMS)
• Random walk:   < 0.04 mg/√Hz (RMS)
• Bandwidth:   >100 Hz>100 Hz

Physical Characteristics

• Misalignment:   <5 arc.min
• Misalignment stability:   <2 arc.min
• Power supply:   27 VDC
• Digital output interface:   RS422
• Operation temperature:   -40°C ~ +60°C
• Dimensions:   215x 217 x 175 mm
• Weight:   5 kg

The export of IFOS-1001 is under strict government control due to its precision characteristics. Export license is granted upon the International Import Certificate (End Use Certificate) issued by the authorized Ministry of the end user’s country and the end use certificate issued by the ultimate end user reflecting the detailed intended civil end use of the Goods. Besides that, the end user company undertakes to grant the right to inspect the Goods supplied at any time. Please allow 2-3 months for the process; positive outcome is not guaranteed even in case all the required documents are presented.

Pure SINS performance (inertial mode, RMS)

• position accuracy: 1.6 km
• velocity accuracy: 0.04 km/h
• Heading accuracy: <0.03 sec(lat)°
• Pitch and roll accuracy: <0.02°

GPS-GLONASS/SINS performance (RMS)

• position accuracy 20 m
• velocity accuracy 0.1 m/sec

Initialization time: 15 min
Gyro bias drift (1s): ≤ 0.01 °/h
Accelerometer bias drift (1s): ≤ 1×10–5g
Interfaces:   MIL-STD-1553B or RS-422/485
Power supply: 27 V DC
Power consumption: 20 W
Size:   171x224x252 mm
Weight:   6.4 kg
Operating ranges

• angular rate: ±550 °/sec
• linear accelerations: to 10 g
• vibration: to 2000 Hz
• thermal operating range: -40 °C to +60 °C

The export of NavFOS-1001 is under strict government control due to its precision characteristics. Export license is granted upon the International Import Certificate (End Use Certificate) issued by the authorized Ministry of the end user’s country and the end use certificate issued by the ultimate end user reflecting the detailed intended civil end use of the Goods. Besides that, the end user company undertakes to grant the right to inspect the Goods supplied at any time. Please allow 2-3 months for the process; positive outcome is not guaranteed even in case all the required documents are presented.