| MOQ: | 1 set |
| Price: | $1000-$100000 |
| Delivery Period: | 30 work days |
| Payment Method: | T/T |
| Supply Capacity: | 500 sets per year |
The Merak-IMU03 Inertial Measurement Unit (IMU) features a strapdown optical design with an integrated gyroscope and accelerometer core. Utilizing intelligent error compensation algorithms, the system delivers standardized real-time motion and orientation data, ensuring high-precision performance for various applications.
Applications:
Missile guidance systems
Pod and platform stabilization
Motion control and navigation systems
Key Advantages:
Precision performance for critical missions
All-solid-state reliability with no moving parts
Instant startup for rapid operational readiness
Optimized SWaP (Size, Weight, Power) characteristics
Long operational lifespan for continuous use
Keywords: Merak-IMU03, 50ppm optical IMU, real-time inertial measurement unit, gyroscope accelerometer IMU, strapdown optical gyro IMU, missile guidance IMU, pod stabilization IMU, motion control IMU, high-precision IMU sensor
| Model | Merak-IMU03 | ||
| Item | indicator | Description | Parameter |
| Gyro | Zero bias | Bias stability (10s) | 0.03°/h |
| Zero bias stability at variable temperature (100s) | 0.1°/h | ||
| Scaling Factor | Scale factor nonlinearity | ≤20ppm | |
| Other indicators | Random walk coefficient | 0.005°/½h | |
| Input range | 400°/s | ||
| Accelerometer | Deviation | Zero bias repeatability | 50μg |
| Zero bias | Bias temperature sensitivity | 50μg/℃ | |
| Scaling Factor | Scale factor repeatability | 50ppm | |
| Scale factor temperature sensitivity | 50ppm/℃ | ||
| Range indicators | Input range | ±20g | |
| Features | Environmental performance | Operating temperature | -40℃~60℃ |
| Storage temperature | -45℃~70℃ | ||
| General Requirements | Power supply | 18~36V(DC) | |
| Stable power consumption | ≤16W | ||
| Mounting hole diameter | 4-Φ4.5mm | ||
| Dimensions(mm) | 110*110*100 | ||
| Weight | ≤1700g | ||
| MOQ: | 1 set |
| Price: | $1000-$100000 |
| Delivery Period: | 30 work days |
| Payment Method: | T/T |
| Supply Capacity: | 500 sets per year |
The Merak-IMU03 Inertial Measurement Unit (IMU) features a strapdown optical design with an integrated gyroscope and accelerometer core. Utilizing intelligent error compensation algorithms, the system delivers standardized real-time motion and orientation data, ensuring high-precision performance for various applications.
Applications:
Missile guidance systems
Pod and platform stabilization
Motion control and navigation systems
Key Advantages:
Precision performance for critical missions
All-solid-state reliability with no moving parts
Instant startup for rapid operational readiness
Optimized SWaP (Size, Weight, Power) characteristics
Long operational lifespan for continuous use
Keywords: Merak-IMU03, 50ppm optical IMU, real-time inertial measurement unit, gyroscope accelerometer IMU, strapdown optical gyro IMU, missile guidance IMU, pod stabilization IMU, motion control IMU, high-precision IMU sensor
| Model | Merak-IMU03 | ||
| Item | indicator | Description | Parameter |
| Gyro | Zero bias | Bias stability (10s) | 0.03°/h |
| Zero bias stability at variable temperature (100s) | 0.1°/h | ||
| Scaling Factor | Scale factor nonlinearity | ≤20ppm | |
| Other indicators | Random walk coefficient | 0.005°/½h | |
| Input range | 400°/s | ||
| Accelerometer | Deviation | Zero bias repeatability | 50μg |
| Zero bias | Bias temperature sensitivity | 50μg/℃ | |
| Scaling Factor | Scale factor repeatability | 50ppm | |
| Scale factor temperature sensitivity | 50ppm/℃ | ||
| Range indicators | Input range | ±20g | |
| Features | Environmental performance | Operating temperature | -40℃~60℃ |
| Storage temperature | -45℃~70℃ | ||
| General Requirements | Power supply | 18~36V(DC) | |
| Stable power consumption | ≤16W | ||
| Mounting hole diameter | 4-Φ4.5mm | ||
| Dimensions(mm) | 110*110*100 | ||
| Weight | ≤1700g | ||