| MOQ: | 1 set |
| Payment Method: | ,T/T |
This high-precision three-axis rotary table is designed for gyroscope and IMU (Inertial Measurement Unit) calibration and dynamic motion simulation. It provides smooth, accurate rotation with high angular rate stability and excellent repeatability, making it ideal for aerospace, UAV, and defense applications. The rugged mechanical design ensures stability under varying loads, while the integrated control system and user-friendly interface enable easy integration with testing workflows.
High-precision 3-axis control
Accurate angular rate and positioning
Supports complex motion profiles (position, rate, and swing modes)
Load adaptability
Stable performance under varying payloads
Mid to high angular speed range
Supports both calibration and dynamic simulation tasks
High-speed dynamic simulation
Enables precise trajectory emulation for aerospace and navigation systems
Reliable calibration
Ideal for gyroscopes, accelerometers, IMUs, optical guidance systems, and communication antennas
Ensures repeatable and reliable testing under extreme conditions
Modular mechanical design for easy maintenance
North prism and counterweight system for balance
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
Integrated aerial plug and base for stable installation
One-click device identification
Accurate and efficient trajectory planning
Real-time motion control adjustment
Full-function test 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 high-precision three-axis rotary table is designed for gyroscope and IMU (Inertial Measurement Unit) calibration and dynamic motion simulation. It provides smooth, accurate rotation with high angular rate stability and excellent repeatability, making it ideal for aerospace, UAV, and defense applications. The rugged mechanical design ensures stability under varying loads, while the integrated control system and user-friendly interface enable easy integration with testing workflows.
High-precision 3-axis control
Accurate angular rate and positioning
Supports complex motion profiles (position, rate, and swing modes)
Load adaptability
Stable performance under varying payloads
Mid to high angular speed range
Supports both calibration and dynamic simulation tasks
High-speed dynamic simulation
Enables precise trajectory emulation for aerospace and navigation systems
Reliable calibration
Ideal for gyroscopes, accelerometers, IMUs, optical guidance systems, and communication antennas
Ensures repeatable and reliable testing under extreme conditions
Modular mechanical design for easy maintenance
North prism and counterweight system for balance
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
Integrated aerial plug and base for stable installation
One-click device identification
Accurate and efficient trajectory planning
Real-time motion control adjustment
Full-function test 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) |