| MOQ: | 1 set |
| Payment Method: | T/T |
The high-accuracy rate table is specifically designed for testing and calibrating inertial navigation systems (INS), including gyroscopes, accelerometers, and optical guidance components. It supports dynamic motion simulation for aerospace, UAV, marine, and defense applications. With smooth rotation, stable performance, and robust construction, it ensures reliable IMU and gyroscope testing under demanding operational conditions.
This system integrates advanced multi-axis motion control with dynamic environmental simulation, enabling precise trajectory emulation and rigorous performance testing.
Ensures accurate angular rate and positioning precision
Supports complex motion simulation (position, rate, and swing modes)
Capable of accommodating a wide range of payloads for sensors and devices
Supports both slow-speed calibration and high-speed dynamic simulation
Accurate reproduction of real-world motion profiles for aerospace and marine environments
Ideal for INS, gyroscopes, accelerometers, optical guidance systems, and communication antennas
Ensures device stability and repeatability under extreme conditions
| 1. Load Installation | |
| - Dimensions (min) | 400 mm (L) × 400 mm (W) × 350 mm (H) |
| - Mass Range (incl. fixtures) | 1 kg ~ 40 kg |
| - Max Load Inertia | 0.4 kg•m² |
| 2. Structural Requirements | |
| - Rotation Angle | Continuous infinite rotation |
| - Structure Type | UOO |
| - Three-Axis Perpendicularity | ≤ ±2 arcsec |
| - Three-Axis Intersection | ≤ Ø0.5 mm sphere |
| - Inner Frame Mounting Surface Flatness | ≤ 0.02 mm |
| - Axis Tilt Rotation Accuracy | ±2 arcsec |
| - Reference Prism (North Guidance) | Mounting accuracy ≤ ±5 arcsec |
| - Locking Mechanism | Middle frame: Mechanical lock |
| Inner/Middle/Outer axes: Electromagnetic locks | |
| - Horizontal Adjustment Range | Ensures installation adjustment accuracy ≤ ±2 arcsec |
| 3. Position Indicators | |
| - Angular Position Accuracy | ±2 arcsec |
| - Angular Repeatability | ±1 arcsec |
| - Angular Resolution | 0.36 arcsec |
| 4. Angular Velocity | |
| - Range: | |
| Outer Axis | ±0.001°/s ~ ±500°/s |
| Middle Axis | ±0.001°/s ~ ±600°/s |
| Inner Axis | ±0.001°/s ~ ±1000°/s |
| Max 3-Axis Linkage | ±60°/s |
| - Accuracy: | |
| ω ≥ 10°/s | 0.00001 (360° avg) |
| 1°/s ≤ ω < 10°/s | 0.0001 (10° avg) |
| ω < 1°/s | 0.001 (1° avg) |
| - Stability: | |
| ω ≥ 10°/s | 0.00001 (360° avg) |
| 1°/s ≤ ω < 10°/s | 0.0001 (10° avg) |
| ω < 1°/s | 0.001 (1° avg) |
| 5. Max Angular Acceleration | |
| - Outer Axis (with load) | 100°/s² |
| - Middle Axis (with load) | 200°/s² |
| - Inner Axis (with load) | 300°/s² |
| 6. Swing Function | |
| - Formula | a=A(2πf)2a=A(2πf)2 |
| Where: a = acceleration, A = amplitude, f = frequency | |
| - Swing Frequencies | 6 Hz, 8 Hz, 10 Hz (limited by max acceleration) |
| MOQ: | 1 set |
| Payment Method: | T/T |
The high-accuracy rate table is specifically designed for testing and calibrating inertial navigation systems (INS), including gyroscopes, accelerometers, and optical guidance components. It supports dynamic motion simulation for aerospace, UAV, marine, and defense applications. With smooth rotation, stable performance, and robust construction, it ensures reliable IMU and gyroscope testing under demanding operational conditions.
This system integrates advanced multi-axis motion control with dynamic environmental simulation, enabling precise trajectory emulation and rigorous performance testing.
Ensures accurate angular rate and positioning precision
Supports complex motion simulation (position, rate, and swing modes)
Capable of accommodating a wide range of payloads for sensors and devices
Supports both slow-speed calibration and high-speed dynamic simulation
Accurate reproduction of real-world motion profiles for aerospace and marine environments
Ideal for INS, gyroscopes, accelerometers, optical guidance systems, and communication antennas
Ensures device stability and repeatability under extreme conditions
| 1. Load Installation | |
| - Dimensions (min) | 400 mm (L) × 400 mm (W) × 350 mm (H) |
| - Mass Range (incl. fixtures) | 1 kg ~ 40 kg |
| - Max Load Inertia | 0.4 kg•m² |
| 2. Structural Requirements | |
| - Rotation Angle | Continuous infinite rotation |
| - Structure Type | UOO |
| - Three-Axis Perpendicularity | ≤ ±2 arcsec |
| - Three-Axis Intersection | ≤ Ø0.5 mm sphere |
| - Inner Frame Mounting Surface Flatness | ≤ 0.02 mm |
| - Axis Tilt Rotation Accuracy | ±2 arcsec |
| - Reference Prism (North Guidance) | Mounting accuracy ≤ ±5 arcsec |
| - Locking Mechanism | Middle frame: Mechanical lock |
| Inner/Middle/Outer axes: Electromagnetic locks | |
| - Horizontal Adjustment Range | Ensures installation adjustment accuracy ≤ ±2 arcsec |
| 3. Position Indicators | |
| - Angular Position Accuracy | ±2 arcsec |
| - Angular Repeatability | ±1 arcsec |
| - Angular Resolution | 0.36 arcsec |
| 4. Angular Velocity | |
| - Range: | |
| Outer Axis | ±0.001°/s ~ ±500°/s |
| Middle Axis | ±0.001°/s ~ ±600°/s |
| Inner Axis | ±0.001°/s ~ ±1000°/s |
| Max 3-Axis Linkage | ±60°/s |
| - Accuracy: | |
| ω ≥ 10°/s | 0.00001 (360° avg) |
| 1°/s ≤ ω < 10°/s | 0.0001 (10° avg) |
| ω < 1°/s | 0.001 (1° avg) |
| - Stability: | |
| ω ≥ 10°/s | 0.00001 (360° avg) |
| 1°/s ≤ ω < 10°/s | 0.0001 (10° avg) |
| ω < 1°/s | 0.001 (1° avg) |
| 5. Max Angular Acceleration | |
| - Outer Axis (with load) | 100°/s² |
| - Middle Axis (with load) | 200°/s² |
| - Inner Axis (with load) | 300°/s² |
| 6. Swing Function | |
| - Formula | a=A(2πf)2a=A(2πf)2 |
| Where: a = acceleration, A = amplitude, f = frequency | |
| - Swing Frequencies | 6 Hz, 8 Hz, 10 Hz (limited by max acceleration) |