Products
PRODUCTS DETAILS
Home > Products >
SIF‑98H Single‑Axis FOG | 0.01°/h Zero‑Bias Stability for Positioning & Orientation

SIF‑98H Single‑Axis FOG | 0.01°/h Zero‑Bias Stability for Positioning & Orientation

MOQ: 1set
Delivery Period: 4-6 weeks
Payment Method: L/C,D/A,D/P,T/T,Western Union
Detail Information
Brand Name
SI
Model Number
SIF-98H
Bias Stability:
≤0.01(°)/h
Measurementaxis:
Single Axis
Application:
Motion Sensing, Navigation, Stabilization
Technology:
Fiber Optic Gyroscope
Grade:
Industrial
Productname:
Single Axis Gyroscope
Highlight:

Single Axis Gyroscope with 0.01°/h stability

,

SIF-98H FOG for positioning

,

Single-Axis FOG orientation sensor

Product Description

This fiber‑optic gyroscope is an inertial angular velocity sensor built upon the Sagnac effect, which measures the carrier’s rotational angular velocity along the sensitive axis. Adopting a digital closed‑loop detection circuit, it captures the optical‑path difference of counter‑propagating light inside the fiber coil induced by external rotational angular velocity. The optical‑path difference is converted into a voltage signal for modulation and demodulation. Closed‑loop feedback and control are implemented to realize real‑time angular‑velocity detection.

Function The product comprises an optical angular‑velocity sensitive unit and a signal‑detection unit. It outputs angle increment data as well as internal temperature information.

Application Areas It is widely used for photoelectric cranes, flying platforms, transportation equipment, inertial navigation systems, inertial measurement systems, optical and photographic instruments, platform stabilization devices and other inertial‑measurement‑related applications.

System Components Main components are listed below: ‑ Optical components: SLD light source, optical fiber coil, integrated optical phase modulator, optical fiber coupler and photodetector; ‑ Circuit section: light‑source driving circuit, signal detection and control circuit; ‑ Gyro mechanical structure.

Size and Installation Dimensions Overall dimensions (mm): 98 ± 0.2 * 98 ± 0.2 * 33.5 ± 0.2 (L * W * H) Installation dimensions (mm): 80 ± 0.1 * 80 ± 0.1 (L * W), 4 * Φ5.4 mm mounting holes

Main performance Parameters

order number

test item

unit

technical requirement

1

Dimension

mm

98*98*33.5

2

Turn-on time

s

3

3

Bias

(°)/h

≤0.3

4

Fixed temperature (constant temperature) bias stability (10s smoothing)

(°)/h

≤0.01

5

Variable temperature bias stability

(1℃ / min variable temperature, 100s smoothing)

(°)/h

≤0.01

6

Bias repeatability

(°)/h

≤0.003

7

Biase magnetic sensitivity

(°)/h /Gs

≤0.005

8

Random walk coefficient

(º)/h1/2

≤0.0005

9

Scale factor nonlinearity

ppm

≤5

10

Scale-factor asymmetry

ppm

≤2

11

Scaling factor repeatability

ppm

≤5

12

Threshold

(°)/h

≤0.003

13

Resolution

(°)/h

≤0.003

14

Width

Hz

≥200

15

Operating temperature

-45~+70

16

Storage temperature

-55~+85

17

Dynamic range

(°)/s

±500

18

Supply voltage

V

+5

19

Steady state power consumption

W

≤2.5

20

Full temperature steady state power consumption

W

≤4

21

Instantaneous starting current

A

<1.5

SIF‑98H Single‑Axis FOG | 0.01°/h Zero‑Bias Stability for Positioning & Orientation


Products
PRODUCTS DETAILS
SIF‑98H Single‑Axis FOG | 0.01°/h Zero‑Bias Stability for Positioning & Orientation
MOQ: 1set
Delivery Period: 4-6 weeks
Payment Method: L/C,D/A,D/P,T/T,Western Union
Detail Information
Brand Name
SI
Model Number
SIF-98H
Bias Stability:
≤0.01(°)/h
Measurementaxis:
Single Axis
Application:
Motion Sensing, Navigation, Stabilization
Technology:
Fiber Optic Gyroscope
Grade:
Industrial
Productname:
Single Axis Gyroscope
Minimum Order Quantity:
1set
Delivery Time:
4-6 weeks
Payment Terms:
L/C,D/A,D/P,T/T,Western Union
Highlight

Single Axis Gyroscope with 0.01°/h stability

,

SIF-98H FOG for positioning

,

Single-Axis FOG orientation sensor

Product Description

This fiber‑optic gyroscope is an inertial angular velocity sensor built upon the Sagnac effect, which measures the carrier’s rotational angular velocity along the sensitive axis. Adopting a digital closed‑loop detection circuit, it captures the optical‑path difference of counter‑propagating light inside the fiber coil induced by external rotational angular velocity. The optical‑path difference is converted into a voltage signal for modulation and demodulation. Closed‑loop feedback and control are implemented to realize real‑time angular‑velocity detection.

Function The product comprises an optical angular‑velocity sensitive unit and a signal‑detection unit. It outputs angle increment data as well as internal temperature information.

Application Areas It is widely used for photoelectric cranes, flying platforms, transportation equipment, inertial navigation systems, inertial measurement systems, optical and photographic instruments, platform stabilization devices and other inertial‑measurement‑related applications.

System Components Main components are listed below: ‑ Optical components: SLD light source, optical fiber coil, integrated optical phase modulator, optical fiber coupler and photodetector; ‑ Circuit section: light‑source driving circuit, signal detection and control circuit; ‑ Gyro mechanical structure.

Size and Installation Dimensions Overall dimensions (mm): 98 ± 0.2 * 98 ± 0.2 * 33.5 ± 0.2 (L * W * H) Installation dimensions (mm): 80 ± 0.1 * 80 ± 0.1 (L * W), 4 * Φ5.4 mm mounting holes

Main performance Parameters

order number

test item

unit

technical requirement

1

Dimension

mm

98*98*33.5

2

Turn-on time

s

3

3

Bias

(°)/h

≤0.3

4

Fixed temperature (constant temperature) bias stability (10s smoothing)

(°)/h

≤0.01

5

Variable temperature bias stability

(1℃ / min variable temperature, 100s smoothing)

(°)/h

≤0.01

6

Bias repeatability

(°)/h

≤0.003

7

Biase magnetic sensitivity

(°)/h /Gs

≤0.005

8

Random walk coefficient

(º)/h1/2

≤0.0005

9

Scale factor nonlinearity

ppm

≤5

10

Scale-factor asymmetry

ppm

≤2

11

Scaling factor repeatability

ppm

≤5

12

Threshold

(°)/h

≤0.003

13

Resolution

(°)/h

≤0.003

14

Width

Hz

≥200

15

Operating temperature

-45~+70

16

Storage temperature

-55~+85

17

Dynamic range

(°)/s

±500

18

Supply voltage

V

+5

19

Steady state power consumption

W

≤2.5

20

Full temperature steady state power consumption

W

≤4

21

Instantaneous starting current

A

<1.5

SIF‑98H Single‑Axis FOG | 0.01°/h Zero‑Bias Stability for Positioning & Orientation