| MOQ: | 1 set |
| Payment Method: | T/T |
This aerospace-grade rate table is designed for high-performance verification and calibration of inertial navigation systems (INS), including gyroscopes, accelerometers, and optical guidance components. It provides ultra-precise angular rate control, smooth operation, and long-term reliability, making it ideal for aviation, marine, and UAV applications.
The system integrates advanced multi-axis motion control with dynamic environmental simulation, enabling accurate trajectory emulation and rigorous operational testing under extreme conditions.
High-precision 3-axis control
Ensures accurate angular rate and positioning
Supports complex motion simulation: position, rate, and swing modes
High load adaptability
Stable performance with varying payloads
Wide angular speed range
Supports both low-speed calibration and high-speed dynamic simulation
High-speed dynamic simulation
Enables precise trajectory emulation for aerospace, defense, and marine environments
Reliable INS calibration
Ideal for gyroscopes, accelerometers, optical guidance systems, and communication antennas
Ensures repeatable and stable testing under extreme conditions
Modular mechanical design for easy maintenance
Multiple safety protections for secure operation
Real-time monitoring and precise motion control
Self-checking and self-calibration for intelligent, stable operation
Industrial-grade control computer for high performance and reliability
One-click device identification
Accurate and efficient trajectory planning
Real-time motion control adjustments
Full-function testing infrastructure
User-friendly human-machine interface
Intelligent early warning and fault handling system
| 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 |
This aerospace-grade rate table is designed for high-performance verification and calibration of inertial navigation systems (INS), including gyroscopes, accelerometers, and optical guidance components. It provides ultra-precise angular rate control, smooth operation, and long-term reliability, making it ideal for aviation, marine, and UAV applications.
The system integrates advanced multi-axis motion control with dynamic environmental simulation, enabling accurate trajectory emulation and rigorous operational testing under extreme conditions.
High-precision 3-axis control
Ensures accurate angular rate and positioning
Supports complex motion simulation: position, rate, and swing modes
High load adaptability
Stable performance with varying payloads
Wide angular speed range
Supports both low-speed calibration and high-speed dynamic simulation
High-speed dynamic simulation
Enables precise trajectory emulation for aerospace, defense, and marine environments
Reliable INS calibration
Ideal for gyroscopes, accelerometers, optical guidance systems, and communication antennas
Ensures repeatable and stable testing under extreme conditions
Modular mechanical design for easy maintenance
Multiple safety protections for secure operation
Real-time monitoring and precise motion control
Self-checking and self-calibration for intelligent, stable operation
Industrial-grade control computer for high performance and reliability
One-click device identification
Accurate and efficient trajectory planning
Real-time motion control adjustments
Full-function testing infrastructure
User-friendly human-machine interface
Intelligent early warning and fault handling system
| 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) |