| MOQ: | 1 set |
| Price: | $1000-$100000 |
| Delivery Period: | 30 work days |
| Payment Method: | T/T |
| Supply Capacity: | 500 sets per year |
The Merak-IMU1 Military Optical IMU is a high-precision strapdown inertial measurement unit integrating gyroscopes and accelerometers in a ruggedized architecture. With advanced error compensation, the system delivers real-time motion data suitable for missile guidance systems, targeting pods, and stabilization platforms.
Applications:
Missile guidance systems
Targeting and sensor pods
Stabilized platforms for military operations
Performance Advantages:
Exceptional accuracy with adaptable design options
All-solid-state reliability with no moving parts
Instant operation readiness for rapid deployment
Optimized SWaP-C (Size, Weight, Power, and Cost) characteristics
Extended operational lifespan for mission-critical applications
Keywords: Merak-IMU1, military optical IMU, inertial measurement unit, gyroscope missile guidance, strapdown IMU, high-precision IMU sensor, targeting pod navigation, stabilized platform IMU, real-time motion data IMU
| Model | Merak-IMU1 | ||
| Item | indicator | Description | Parameter |
| Gyro | Zero bias | Bias stability (10s) | 0.005°/h |
| Zero bias stability at variable temperature (100s) | 0.02°/h | ||
| Scaling Factor | Scale factor nonlinearity | ≤20ppm | |
| Other indicators | Random walk coefficient | 0.0005°/½h | |
| Input range | 400°/s | ||
| Accelerometer | Deviation | Zero bias repeatability | 20μg |
| Zero bias | Bias temperature sensitivity | 20μg/℃ | |
| Scaling Factor | Scale factor repeatability | 20ppm | |
| Scale factor temperature sensitivity | 20ppm/℃ | ||
| 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-Φ5.5mm | ||
| Dimensions(mm) | 130*130*110 | ||
| Weight | ≤2200g | ||
| MOQ: | 1 set |
| Price: | $1000-$100000 |
| Delivery Period: | 30 work days |
| Payment Method: | T/T |
| Supply Capacity: | 500 sets per year |
The Merak-IMU1 Military Optical IMU is a high-precision strapdown inertial measurement unit integrating gyroscopes and accelerometers in a ruggedized architecture. With advanced error compensation, the system delivers real-time motion data suitable for missile guidance systems, targeting pods, and stabilization platforms.
Applications:
Missile guidance systems
Targeting and sensor pods
Stabilized platforms for military operations
Performance Advantages:
Exceptional accuracy with adaptable design options
All-solid-state reliability with no moving parts
Instant operation readiness for rapid deployment
Optimized SWaP-C (Size, Weight, Power, and Cost) characteristics
Extended operational lifespan for mission-critical applications
Keywords: Merak-IMU1, military optical IMU, inertial measurement unit, gyroscope missile guidance, strapdown IMU, high-precision IMU sensor, targeting pod navigation, stabilized platform IMU, real-time motion data IMU
| Model | Merak-IMU1 | ||
| Item | indicator | Description | Parameter |
| Gyro | Zero bias | Bias stability (10s) | 0.005°/h |
| Zero bias stability at variable temperature (100s) | 0.02°/h | ||
| Scaling Factor | Scale factor nonlinearity | ≤20ppm | |
| Other indicators | Random walk coefficient | 0.0005°/½h | |
| Input range | 400°/s | ||
| Accelerometer | Deviation | Zero bias repeatability | 20μg |
| Zero bias | Bias temperature sensitivity | 20μg/℃ | |
| Scaling Factor | Scale factor repeatability | 20ppm | |
| Scale factor temperature sensitivity | 20ppm/℃ | ||
| 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-Φ5.5mm | ||
| Dimensions(mm) | 130*130*110 | ||
| Weight | ≤2200g | ||