• White background shot of Inertial Navigation Test Table with three axis design for precision aerospace calibration
  • Side view of Inertial Navigation Test Table showing rigid frame for high load rotary testing
  • Close-up of Inertial Navigation Test Table high precision bearing assembly ensuring smooth motion
  • Inertial Navigation Test Table operating in lab calibrating UAV inertial navigation system
  • Size comparison of Inertial Navigation Test Table next to standard industrial workbench for scale
  • Functional demo of Inertial Navigation Test Table simulating flight motion for gyro calibration
  • White background shot of Inertial Navigation Test Table with three axis design for precision aerospace calibration
  • Side view of Inertial Navigation Test Table showing rigid frame for high load rotary testing
  • Close-up of Inertial Navigation Test Table high precision bearing assembly ensuring smooth motion
  • Inertial Navigation Test Table operating in lab calibrating UAV inertial navigation system
  • Size comparison of Inertial Navigation Test Table next to standard industrial workbench for scale
  • Functional demo of Inertial Navigation Test Table simulating flight motion for gyro calibration

High Precision Three Axis Rate Table for Aerospace and Defense Multi Axis Test

No.BE-INS3-23B06
This high precision three axis rate table serves as motion simulator and gyro test stand for aerospace and defense multi-axis dynamic testing. 20kg load capacity with Φ360mm stainless platform supports missile guidance components and flight control sensors. Ideal for missile guidance system validation, aircraft attitude control simulation, radar servo system testing, and defense equipment performance verification under high dynamic conditions.
Specifications
Rated Load Weight:
20 kg
Three-Axis Position Accuracy:
≤ ±5″
Maximum Angular Rate Range:
±500°/s
Maximum Angular Acceleration:
300°/s²
Three-Axis Rate Accuracy and Stability:
5×10⁻³ (1° average)
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  • White background shot of Inertial Navigation Test Table with three axis design for precision aerospace calibration
  • Side view of Inertial Navigation Test Table showing rigid frame for high load rotary testing
  • Close-up of Inertial Navigation Test Table high precision bearing assembly ensuring smooth motion
  • Inertial Navigation Test Table operating in lab calibrating UAV inertial navigation system
  • Size comparison of Inertial Navigation Test Table next to standard industrial workbench for scale
  • Functional demo of Inertial Navigation Test Table simulating flight motion for gyro calibration

Description

Technical Specifications
2.1 Countertop and Load
Rated Load Weight 20 kg
Maximum Load Dimensions Φ300 mm × 200 mm
Countertop (Mounting Surface) Φ360 mm, Stainless Steel
Countertop Flatness ≤ 0.02 mm
Countertop Face Runout ≤ 0.02 mm
Countertop Mounting Screw Holes M6, Pitch 25 mm
2.2 Main Technical Specifications
Three-Axis Position Accuracy ≤ ±5″
Three-Axis Angular Position Repeatability ≤ ±3″
Three-Axis Rotation Axis Perpendicularity ≤ ±5″
Three-Axis Rotation Angle Range 360° Continuous Rotation
Three-Axis Rotation Axis Intersection Accuracy Within a Φ0.5 mm Sphere
Equipment Weight Approx. 120 kg
Maximum Angular Rate Range Inner Frame: ±500°/s
Middle Frame: ±400°/s
Outer Frame: ±300°/s
Three-Axis Linkage: ±100°/s
Maximum Angular Acceleration Inner Frame: 300°/s²
Middle Frame: 200°/s²
Outer Frame: 100°/s²
Three-Axis Rate Accuracy and Stability 5×10⁻⁵ (360° average)
5×10⁻⁴ (10° average)
5×10⁻³ (1° average)
Slip Ring Total 30 channels:
• 14 single-core, rated current 3 A
• 16 twisted-pair shielded lines, rated current 2 A
Control Software Computer-automated status control, data acquisition, processing, and display
Communication Interface RS232 / RS422
2.3 Operating Environment
Power Supply 220 V ±10% / 50 Hz
Ambient Temperature -10 ℃ to 35 ℃
Relative Humidity ≤ 80% RH