CSSC Star&Inertia Technology co.,ltd.
| Supply Ability | 500 sets per year |
| Delivery Time | 7work days |
| Payment Terms | T/T |
| Packaging Details | 30cm*30cm*28cm |
| Accelerometer/Months Bias Repeatability（1σ） | ≤20μg |
| Accelerometer/Months Scale Factor Accuracy（1σ） | ≤20ppm |
| Gyro/Bias Repeatability（1σ） | ≤0.008°/hr |
| Gyro/Scale Factor Accuracy（1σ） | ≤20ppm |
| Gyro/Random walk（1σ） | ≤0.003°/√hr |
| Position accuracy/Pure inertia | ≤0.8nm/1h |
| Position accuracy/Inertial navigation satellite combination | better than satellite accuracy |
| Speed accuracy/Pure inertia | ≤1.0m/s |
| Speed accuracy/Inertial navigation satellite combination | ≤0.2m/s |
| Angular Rate | ≥±400°/sec |
| Angular Acceleration | 100000°/sec2 |
| Acceleration | ＞25g |
| Angular Attitude | Any Orientation |
| Alignment time | ≤8min |
| Input/output | 3 RS422 full-duplex serial ports, 1 100M Ethernet port |
| Heading Accuracy/Pure inertia | ≤0.1°sec(L) |
| Heading Accuracy/Satellite navigation combination | ≤0.05°sec(L) |
| Pitch & Roll Accuracy/Pure inertia | ≤0.03° |
| Pitch & Roll Accuracy/Satellite navigation combination | ≤0.015° |
| Power consumption | ＜20W |
| Dimensions | 195×160×108mm |
| Weight | ＜3.9kg |
| Temperature | -40℃~70℃ |
| Shock | 15g，Half-sine wave 11ms |
| Input Voltage | DC24V(±25%) |
| cooling | Conduction to mounting plate |
| Vibration | 20~2000Hz,6.06g |
| MTBF | ＞25000 hours |
| Brand Name | Star & Inertia Technology |
| Model Number | F3AAA |
| Place of Origin | China |
| Certification | GJN485963217 |
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Product Specification
| Supply Ability | 500 sets per year | Delivery Time | 7work days |
| Payment Terms | T/T | Packaging Details | 30cm*30cm*28cm |
| Accelerometer/Months Bias Repeatability（1σ） | ≤20μg | Accelerometer/Months Scale Factor Accuracy（1σ） | ≤20ppm |
| Gyro/Bias Repeatability（1σ） | ≤0.008°/hr | Gyro/Scale Factor Accuracy（1σ） | ≤20ppm |
| Gyro/Random walk（1σ） | ≤0.003°/√hr | Position accuracy/Pure inertia | ≤0.8nm/1h |
| Position accuracy/Inertial navigation satellite combination | better than satellite accuracy | Speed accuracy/Pure inertia | ≤1.0m/s |
| Speed accuracy/Inertial navigation satellite combination | ≤0.2m/s | Angular Rate | ≥±400°/sec |
| Angular Acceleration | 100000°/sec2 | Acceleration | ＞25g |
| Angular Attitude | Any Orientation | Alignment time | ≤8min |
| Input/output | 3 RS422 full-duplex serial ports, 1 100M Ethernet port | Heading Accuracy/Pure inertia | ≤0.1°sec(L) |
| Heading Accuracy/Satellite navigation combination | ≤0.05°sec(L) | Pitch & Roll Accuracy/Pure inertia | ≤0.03° |
| Pitch & Roll Accuracy/Satellite navigation combination | ≤0.015° | Power consumption | ＜20W |
| Dimensions | 195×160×108mm | Weight | ＜3.9kg |
| Temperature | -40℃~70℃ | Shock | 15g，Half-sine wave 11ms |
| Input Voltage | DC24V(±25%) | cooling | Conduction to mounting plate |
| Vibration | 20~2000Hz,6.06g | MTBF | ＞25000 hours |
| Brand Name | Star & Inertia Technology | Model Number | F3AAA |
| Place of Origin | China | Certification | GJN485963217 |
| High Light | aircraft laser inertial navigation system ，airborne optical gyro INS ，tactical grade inertial navigation system | ||
This airborne inertial navigation system is developed using optical gyroscopes and quartz accelerometers as the fundamental sensing elements. The system adopts a strapdown inertial configuration, with optional modulation-based processing, enabling continuous internal navigation computation and real-time output of navigation data.
Optical Gyroscope and Quartz Accelerometer Sensors
Designed to meet the stability and reliability requirements of airborne platforms.
Strapdown Inertial Navigation Architecture
Integrated structure suitable for compact airborne installation and high-rate navigation calculation.
High-Speed Navigation Algorithms
Embedded software processes inertial data efficiently to generate real-time navigation outputs.
Multi-Source Navigation Data Fusion
Supports optional integration of satellite navigation, astronomical reference, altitude data, radio navigation aids, and vision-based information based on operational needs.
Flexible Operation Modes
Capable of operating in standalone inertial navigation mode or multi-source integrated navigation mode.
High Navigation Autonomy
Provides continuous navigation capability independent of external signal availability.
Adaptable Integration Capability
Allows configuration according to mission requirements and sensor availability.
Stable and Real-Time Output
Supplies essential navigation parameters for airborne guidance and control systems.
Compatibility with Avionics Systems
Designed for integration into a wide range of airborne platforms and onboard systems.
Aircraft inertial navigation systems
Navigation and guidance for fixed-wing aircraft, rotary-wing aircraft, and unmanned aerial vehicles (UAVs)
Integrated navigation solutions combining inertial and external reference data
Airborne platforms requiring continuous attitude, heading, velocity, and position information
Flight testing, aviation research, 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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