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Alioth-90 Spacecraft Sagnac Ring Laser Gyroscope For INS Inertial Navigation Systems
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Alioth-90 Spacecraft Sagnac Ring Laser Gyroscope For INS Inertial Navigation Systems
  • name

Alioth-90 Spacecraft Sagnac Ring Laser Gyroscope For INS Inertial Navigation Systems

MOQ: 1 set
Price: $1000-$100000
Delivery Period: 30 work days
Supply Capacity: 1000 sets per year
Details Information
Product Description
Detail Information
Place of Origin
China
Brand Name
Star & Inertia Technology
Model Number
RLG（Alioth-90）
Performance\Bias Stability (1σ):
0.004°/h~0.002°/h
Performance\Zero Bias Repeatability (1σ):
0.002°/h~0.001°/h
Performance\ARW（Angular Random Walk(1σ):
0.0007°/√hr~0.0004°/√hr
Performance\Scale Factor Error (1σ):
≤2ppm
Performance\Dynamic Range:
≥±400°/s
Performance\Bandwidth:
＞200Hz
Electrical Interface\Turn On Time:
＜5s
Electrical Interface\Output Signal Format:
TTL
Electrical Interface\Built In Self-test:
Yes
Electrical Interface\Output Signal Update Rate:
1Hz
Electrical Interface\Output Signal Baud Rate:
115200
Electrical Interface\Vibration Shock:
75g, Half Sine, 6ms
Electrical Interface\Operating Temperature:
- 40℃ ~ + 70℃
Electrical Interface\Storage Temperature:
- 55℃ ~ + 85℃
Physical Specifications\Power Supply:
±15V,±5V
Physical Specifications\Connector (25 Pins):
J30JM-37ZKP36
Physical Specifications\Power Consumption:
≤3W
Physical Specifications\MTBF (per MIL-HDBK-217-F):
＞10000hr
Physical Specifications\Weight:
2kg
Physical Specifications\Dimensions:
151mm×126mm×57mm
Highlight:

Spacecraft Ring Laser Gyroscope

,

Sagnac Ring Laser Gyroscope

,

INS ring gyroscope

Product Description

    RLG(Alioth-90)

The Ring Laser Gyroscope (RLG) operates on the Sagnac effect principle, measuring angular increments by detecting phase differences of laser beams in a closed glass cavity. Featuring high integration, exceptional reliability, strong environmental adaptability and stable performance, it has become the sensor of choice for high-precision inertial navigation systems worldwide. Applications include spacecraft, aircraft, satellites, vehicles, ships and submersibles for navigation and attitude reference.

    Key features: 1) Monolithic optical/electronic packaging for easy installation; 2) Compact, lightweight design with controlled power consumption; 3) High reliability and shock/vibration resistance; 4) Wide dynamic response bandwidth with digital output.

Series RLG  Series
Type Alioth-90
Performance Bias stability (1σ) 0.004°/h~0.002°/h
Zero bias repeatability (1σ) 0.002°/h~0.001°/h
ARW(Angular random walk(1σ) 0.0007°/√hr~0.0004°/√hr
Scale factor error (1σ) ≤2ppm
Dynamic Range ≥±400°/s
Bandwidth ＞200Hz
Electrical Interface Turn on time ＜5s
Output signal format TTL
Built in self-test yes
Output signal update rate 1Hz
Output signal baud rate 115200
Vibration shock 75g, half sine, 6ms
Operating temperature  - 40℃ ~ + 70℃
Storage temperature  - 55℃ ~ + 85℃
Physical Specifications Power supply ±15V,±5V
Connector (25 pins) J30JM-37ZKP36
Power consumption ≤3W
MTBF (per MIL-HDBK-217-F) ＞10000hr
Weight 2kg
Dimensions 151mm×126mm×57mm


Tags: 

ring laser gyro,  

rlg gyro,  

ring gyroscope

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products
PRODUCTS DETAILS
Products

Laser Inertial Navigation System

Fiber Optic Inertial Navigation System

Aircraft Inertial Navigation System

Marine Inertial Navigation System

Automotive Inertial Navigation System

AHRS System

IMU Inertial Measurement Unit

Fiber Optic Gyroscope

Ring Laser Gyroscope
Alioth-90 Spacecraft Sagnac Ring Laser Gyroscope For INS Inertial Navigation Systems
  • name
Alioth-90 Spacecraft Sagnac Ring Laser Gyroscope For INS Inertial Navigation Systems
MOQ: 1 set
Price: $1000-$100000
Delivery Period: 30 work days
Supply Capacity: 1000 sets per year
Detail Information
Product Description
Detail Information
Place of Origin
China
Brand Name
Star & Inertia Technology
Model Number
RLG（Alioth-90）
Performance\Bias Stability (1σ):
0.004°/h~0.002°/h
Performance\Zero Bias Repeatability (1σ):
0.002°/h~0.001°/h
Performance\ARW（Angular Random Walk(1σ):
0.0007°/√hr~0.0004°/√hr
Performance\Scale Factor Error (1σ):
≤2ppm
Performance\Dynamic Range:
≥±400°/s
Performance\Bandwidth:
＞200Hz
Electrical Interface\Turn On Time:
＜5s
Electrical Interface\Output Signal Format:
TTL
Electrical Interface\Built In Self-test:
Yes
Electrical Interface\Output Signal Update Rate:
1Hz
Electrical Interface\Output Signal Baud Rate:
115200
Electrical Interface\Vibration Shock:
75g, Half Sine, 6ms
Electrical Interface\Operating Temperature:
- 40℃ ~ + 70℃
Electrical Interface\Storage Temperature:
- 55℃ ~ + 85℃
Physical Specifications\Power Supply:
±15V,±5V
Physical Specifications\Connector (25 Pins):
J30JM-37ZKP36
Physical Specifications\Power Consumption:
≤3W
Physical Specifications\MTBF (per MIL-HDBK-217-F):
＞10000hr
Physical Specifications\Weight:
2kg
Physical Specifications\Dimensions:
151mm×126mm×57mm
Minimum Order Quantity:
1 set
Price:
$1000-$100000
Delivery Time:
30 work days
Supply Ability:
1000 sets per year
Highlight

Spacecraft Ring Laser Gyroscope

,

Sagnac Ring Laser Gyroscope

,

INS ring gyroscope

Product Description

    RLG(Alioth-90)

The Ring Laser Gyroscope (RLG) operates on the Sagnac effect principle, measuring angular increments by detecting phase differences of laser beams in a closed glass cavity. Featuring high integration, exceptional reliability, strong environmental adaptability and stable performance, it has become the sensor of choice for high-precision inertial navigation systems worldwide. Applications include spacecraft, aircraft, satellites, vehicles, ships and submersibles for navigation and attitude reference.

    Key features: 1) Monolithic optical/electronic packaging for easy installation; 2) Compact, lightweight design with controlled power consumption; 3) High reliability and shock/vibration resistance; 4) Wide dynamic response bandwidth with digital output.

Series RLG  Series
Type Alioth-90
Performance Bias stability (1σ) 0.004°/h~0.002°/h
Zero bias repeatability (1σ) 0.002°/h~0.001°/h
ARW(Angular random walk(1σ) 0.0007°/√hr~0.0004°/√hr
Scale factor error (1σ) ≤2ppm
Dynamic Range ≥±400°/s
Bandwidth ＞200Hz
Electrical Interface Turn on time ＜5s
Output signal format TTL
Built in self-test yes
Output signal update rate 1Hz
Output signal baud rate 115200
Vibration shock 75g, half sine, 6ms
Operating temperature  - 40℃ ~ + 70℃
Storage temperature  - 55℃ ~ + 85℃
Physical Specifications Power supply ±15V,±5V
Connector (25 pins) J30JM-37ZKP36
Power consumption ≤3W
MTBF (per MIL-HDBK-217-F) ＞10000hr
Weight 2kg
Dimensions 151mm×126mm×57mm


Tags: 

ring laser gyro,

rlg gyro,

ring gyroscope

CSSC Star&Inertia Technology co.,ltd.
No. 717, Sunshine Avenue, Jiangxia District, Wuhan City, Hubei Province
Tel: +86-18071128027
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