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Part NO. : | FOG98HB |
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FOG98HB Middle Grade Precision Closed-loop
Fiber Optic Gyroscope
Description
FOG Photonics has developed the FOG600S(FOG98HB) for demanding navigation and sensor pointing under conditions where external aiding signals may not be available. The key features of the FOG600S are the miniature size, separate axes packaged for challenging integration, high update rate for closed loop pointing and tracking, low angle random walk (ARW) to mitigate the effect of platform jitter and low bias drift to enable accurate pointing during platform motion. TheFOG600S’ability to locate the gyro axis on rigid optical or physical structures and our temperature stabilized laser sensing provide superior response for unaided navigation, spatial imaging, laser designation and for optical seeker targeting. These units use very short fiber optic coils coupled with advanced analog and digital electronics and signal processing that achieves update rates greater than 1 kHz, angular random walk better than 0.007 °/√hr and bias drift of less than 0.02 °/hr. The FOG600S offers a standalone configuration with one-to-three separate axes (axis-1 includes system electronics and optics) or as an optional integrated single package. FOGPhotonics is also offering the IMU systems, which is an integrated 3-axis IMU with an overall package weight < 2.5kg and under 15 W power consumption. Additionally, in development is the FOG600 advanced inertial sensor, which will use a breakthrough architecture and manufacturing process to achieve comparable performance in the compact package.
Features
● Closed loop fiber optic gyroscope
● High accuracy, low noise sensor
● All "Solid State" containing no moving parts
● Digital and/or Analog output Available as 1 -2-3-4 axes configuration
● High resolution Low latency Lightweight package
● Temperature modeled Reduced magnetic sensitivity
● Provisions for extra processing capabilities
● Ruggedized packaging
● Great performance with harsh dynamic conditions
Applications
● Navigation
● Missile and Torpedoe guidance
● Flight controls
● UUV/UAV/ Target Drones guidance and control
● Gyro compassing / target acquisition systems
● Camera/mapping
● AHRS
● Motion compensation
● EO/FUR/Radar stabilization
● Line-of-sight tracking / Precision pointing
● Smart munitions
● Gimbal control
Technical Specification
Parameter |
Units |
FOG98HB |
Angular Random Walk (noise)* |
°⁄√hr |
0.001 |
Bias stability |
°/hr |
≤0.02(10s,1σ) ≤0.007(100s,1σ) |
Bias Repeatability (day to day) |
°/hr(1σ) |
0.01 |
Scale factor repeatability |
ppm(1σ) |
≤20(Full temperature) |
Scale Factor Non-Linearity (max rate, 25°C) |
ppm,(1σ) |
≤10 |
Dynamic Range (Angular Rate) |
°/sec |
±600 |
Band width |
HZ |
>100 |
Dimension |
mm |
98x98x35 |
Weight |
g |
<550 |
Operation temperature |
℃ |
-40-+71 |
Storage temperature |
℃ |
-55-+85 |
Shock |
g |
20 g, 11 msec, sawtooth |
Vibrations |
g |
4.2g(20-1500HZ) |
Interface |
|
RS422 Or OEM |
Power supply |
V |
±5V |
MTBF |
Hours |
20000 |
Baud Rate |
Kbps |
Typ 460.8kbps (User selectable 9.6 Kbps to 921.6 Kbps) |
Data Rate |
Hz |
Typ500Hz(User Selectable 1 to 1000 Hz) |
Dimension
Pin-definition and Communication
Closed loop Fiber optic gyro test report
Dimensions of FOG98HB Middle Grade Precision Closed-loop FOG
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