CSSC Star&Inertia Technology co.,ltd.
| Supply Ability | 500 sets per year |
| Delivery Time | 30 work days |
| Accelerometer/Months Bias Repeatability（1σ） | ≤500μg |
| Accelerometer/Months Scale Factor Accuracy（1σ） | ≤500ppm |
| Gyro/Bias Repeatability（1σ） | ≤0.1°/hr |
| Gyro/Scale Factor Accuracy（1σ） | ≤300ppm |
| Gyro/Random walk（1σ） | ≤0.03°/√hr |
| Position accuracy/Pure inertia | ≤1nm/10min |
| Position accuracy/Inertial navigation satellite combination | better than satellite accuracy |
| Speed accuracy/Pure inertia | / |
| Speed accuracy/Inertial navigation satellite combination | ≤0.2m/s |
| Angular Rate | ≥±400°/sec |
| Angular Acceleration | 100000°/sec2 |
| Acceleration | ＞40g |
| Angular Attitude | Any Orientation |
| Alignment time | ≤5min |
| Input/output | 2 RS422 serial ports |
| Heading Accuracy/Pure inertia | / |
| Heading Accuracy/Satellite navigation combination | ≤1°sec(L) |
| Pitch & Roll Accuracy/Pure inertia | / |
| Pitch & Roll Accuracy/Satellite navigation combination | ≤0.2° |
| Power consumption | ＜10W |
| Dimensions | 70×70×53mm |
| Weight | ＜500g |
| Temperature | -40℃~60℃ |
| Shock | 15g，Half-sine wave 11ms |
| Input Voltage | DC24V(±25%) |
| cooling | Conduction to mounting plate |
| Vibration | 20~2000Hz,6.06g |
| MTBF | ＞20000 hours |
| Brand Name | Star & Inertia Technology |
| Model Number | |
| Place of Origin | China |
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Product Specification
| Supply Ability | 500 sets per year | Delivery Time | 30 work days |
| Accelerometer/Months Bias Repeatability（1σ） | ≤500μg | Accelerometer/Months Scale Factor Accuracy（1σ） | ≤500ppm |
| Gyro/Bias Repeatability（1σ） | ≤0.1°/hr | Gyro/Scale Factor Accuracy（1σ） | ≤300ppm |
| Gyro/Random walk（1σ） | ≤0.03°/√hr | Position accuracy/Pure inertia | ≤1nm/10min |
| Position accuracy/Inertial navigation satellite combination | better than satellite accuracy | Speed accuracy/Pure inertia | / |
| Speed accuracy/Inertial navigation satellite combination | ≤0.2m/s | Angular Rate | ≥±400°/sec |
| Angular Acceleration | 100000°/sec2 | Acceleration | ＞40g |
| Angular Attitude | Any Orientation | Alignment time | ≤5min |
| Input/output | 2 RS422 serial ports | Heading Accuracy/Pure inertia | / |
| Heading Accuracy/Satellite navigation combination | ≤1°sec(L) | Pitch & Roll Accuracy/Pure inertia | / |
| Pitch & Roll Accuracy/Satellite navigation combination | ≤0.2° | Power consumption | ＜10W |
| Dimensions | 70×70×53mm | Weight | ＜500g |
| Temperature | -40℃~60℃ | Shock | 15g，Half-sine wave 11ms |
| Input Voltage | DC24V(±25%) | cooling | Conduction to mounting plate |
| Vibration | 20~2000Hz,6.06g | MTBF | ＞20000 hours |
| Brand Name | Star & Inertia Technology | Model Number | |
| Place of Origin | China | ||
| High Light | fiber-optic inertial navigation system ，airborne optical gyro system ，aircraft inertial navigation system with gyro | ||
The airborne optical gyro inertial navigation system is designed with optical gyroscopes and quartz accelerometers as its primary sensing components. Using a strapdown inertial navigation architecture, with optional modulation-based techniques, the system performs high-speed internal navigation computation and delivers navigation data continuously in real time.
Optical Gyro and Quartz Accelerometer Configuration
Provides stable inertial sensing suitable for airborne operating conditions.
Strapdown Inertial Navigation Structure
Compact and integrated design for real-time attitude, velocity, and position calculation.
High-Speed Navigation Processing
Embedded navigation algorithms ensure timely computation and output of navigation parameters.
Multi-Source Navigation Integration
Capable of incorporating external navigation information such as satellite navigation, astronomical reference, altimeters, radio navigation aids, and vision-based data, based on user configuration.
Multiple Operating Modes
Supports pure inertial navigation as well as multi-source integrated navigation and information fusion modes.
Continuous Navigation Capability
Maintains stable navigation output independent of external signal availability.
Flexible Configuration
Information sources and fusion strategies can be adapted to different mission requirements.
Reliable Real-Time Output
Provides consistent navigation data required by airborne guidance and control systems.
Strong System Compatibility
Designed for integration with aircraft avionics and mission management systems.
Aircraft inertial navigation systems
Navigation and guidance for fixed-wing aircraft, helicopters, and UAVs
Integrated navigation systems combining inertial and satellite data
Airborne platforms requiring attitude, heading, velocity, and position information
Aviation research, testing, and specialized airborne missions
Company Details
Business Type:
Manufacturer
Year Established:
2013
Total Annual:
5000000-10000000
Employee Number:
300~500
Ecer Certification：
Verified Supplier
CSSC Star&Inertia Technology co.,ltd. is located in Wuhan, Hubei Province, located in the "Optical Valley of China", backed by the world's largest optical fiber and cable research and development base, the largest domestic optical device research and development and production base... CSSC Star&Inertia Technology co.,ltd. is located in Wuhan, Hubei Province, located in the "Optical Valley of China", backed by the world's largest optical fiber and cable research and development base, the largest domestic optical device research and development and production base...
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