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Model ID-250-5
This gimbal table consists of an inner 3-axis set (simulating roll, pitch and yaw of aircraft) and an outer 2-axis set (simulating target motion). It reproduces the relative motion attitudes between aircraft and targets in the laboratory, providing a hardware-in-the-loop simulation test environment for seeker heads and flight control systems.
Features
- High-precision five-axis synchronous control
- Full aircraft attitude motion simulation
- Real target scenario loading supported
- Dynamic real-time simulation & testing
- High-rigidity frame with fast response
- Suitable for multiple seeker tests
Applications
Ideal for aerospace and defense industries. It is primarily used for hardware-in-the-loop simulation testing and performance evaluation of seekers and flight control systems onboard aircraft such as missiles and UAVs.
Specifications
| Parameter Categories | Parameter Items | Parameter Value |
|---|---|---|
| Accuracy Performance | Angular Position Accuracy | ≤ ±3″ |
| Angular Position Repeatability | ≤ ±2″ | |
| Velocity Flatness | ω < 1°/s: 2e-003 | |
| Dynamic Performance | Maximum Angular Velocity | ≥7200°/s |
| Maximum Angular Acceleration | 200°/s² | |
| Rotational Range | Azimuth: unlimited continuous 360° rotation | |
| Mechanical Specifications | Payload Capacity | 20 kg |
| Table Diameter / Platform Dimensions | Φ360 mm |
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