Equipment Overview
Explore the functions and specifications of the equipment operated by our center at a glance.
Available
AAV Integrated System Ground Test Facility
This facility enables comprehensive pre-flight verification of an aircraft’s integrated systems—including flight control, electrical and electronic systems, and hydraulics—under ground conditions. By validating system functionality prior to actual flight,
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Equipment Details
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Key Feature
- Test Category: AAV Flight Control Performance and Vibration Testing
- AAVs, like conventional aircraft, require performance and reliability evaluation not only at the component level but also as an integrated system.
- Ground Vibration Tests (GVT) are conducted to prevent flutter phenomena that may occur during flight.
- Enables low-altitude ground-based flight tests to evaluate integrated AAV systems such as hovering and attitude control.
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PAV Integrated System Ground Test Facility
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Test in Progress
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Facility Installation Photo
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Structural Layout of the PAV Prototype Ground Testing Facility
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Specification
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Flight Test Jig Used for mounting AAV airframes and performing low-altitude flight tests (5m × 5m × 3.62m / 6 degrees of freedom) Safety Fence Prevents safety accidents during flight testing(10m × 10m × 4.245m) Impact Absorption System Minimizes aircraft damage in the event of a crash during testing Work Table Table for installing aircraft controllers, measurement systems, and related equipment Ground Vibration Test (GVT) System Analyzes natural frequencies of the full airframe(3-axis accelerometers, DAQ, dedicated analysis tools, shaker, bungee cords, etc.) Power Supply Unit Supplies external power to the aircraft when required(up to 250 kW, 800 V)
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