Audited Supplier
AINS-20
Fiber Optic Vertical Gyro
0.1deg (Length of Baseline 2m)
0.05deg
3m (Cep) , 2cm+1ppm(Cep) (Post-Differentiation)
12h
Aircraft Flight Control and Navigation
JOHO
Standard Packing
GJB
China Wuhan
90275000
Product Description
Ship-Borne / Vehicle-Borne Navigation Gyroscope System , Fibre Optic Gyro
Employing high accuracy FOG, Q-flex accelerometers, dual-frequency GPS position & orientation system, barometric altimeter and advanced integration navigation and attitude measurement algorithm, the performance of AINS-10 has been dramatically improved. Combining built-in high accuracy IMU (inertial measurement unit) with satellite, it could output high accuracy position, speed, attitude, angular speed and acceleration information. While the satellite signal is completely covered, system would enter into pure inertial mode. By use of high accuracy FOG, it could still keep good attitude measurement accuracy in certain time. Integrated with barometric altimeter, it could make correction and get higher accuracy height information.
Application
Aircraft flight control and navigation
Ship-borne & vehicle-borne navigation system
Inertial stability control system
E-traffic measurement system
Industrial & agricultural measurement and application
Technical Specifications
Employing high accuracy FOG, Q-flex accelerometers, dual-frequency GPS position & orientation system, barometric altimeter and advanced integration navigation and attitude measurement algorithm, the performance of AINS-10 has been dramatically improved. Combining built-in high accuracy IMU (inertial measurement unit) with satellite, it could output high accuracy position, speed, attitude, angular speed and acceleration information. While the satellite signal is completely covered, system would enter into pure inertial mode. By use of high accuracy FOG, it could still keep good attitude measurement accuracy in certain time. Integrated with barometric altimeter, it could make correction and get higher accuracy height information.
Application
Aircraft flight control and navigation
Ship-borne & vehicle-borne navigation system
Inertial stability control system
E-traffic measurement system
Industrial & agricultural measurement and application
Technical Specifications
| Range | |
| Heading | 0~360°, |
| Pitch angle | ±90° |
| Roll angle | ±180° |
| Angular rate | ±300°/s |
| Acceleration | ±10g |
| Positioning & orientation accuracy | |
| Heading accuracy (GPS valid) | 0.1° (length of baseline 2m, 1σ) |
| Attitude (GPS valid) | 0.05° (1σ) |
| Position accuracy (GPS valid) | 3m (CEP) , 2cm+1ppm(CEP) (post-differentiation) |
| Velocity accuracy (GPS valid) | 0.1m/s (rms), (1σ) |
| Preparation time | |
| Start time | ≤10s |
| Stable time | System working normally after GPS and heading valid (specified time depends on surrounding environment, open field 2min) |
| Power supply | |
| Power supply | DC12~32V, 24V±10% (rating) |
| Power consumption | ≤25W |
| Reliability | |
| MTBF | 2000h |
| Continuous working time | ≥12h |
| Physical parameters | |
| System weight | ≤3.6kg (excluding antenna and feeder line) |
| Physical dimension | 191mm×166mm×131.5mm (X, Y, Z) |
