• White background shot of Inertial Navigation Test Table for fiber optic gyro calibration with three-axis structure
  • Inertial Navigation Test Table shown with full frame design for motion simulation and sensor testing
  • Close-up of Inertial Navigation Test Table high-precision bearing assembly for smooth rotation
  • Inertial Navigation Test Table operating in aerospace lab for UAV inertial sensor calibration
  • Side view of Inertial Navigation Test Table showing compact 60 cm width suitable for labs
  • White background shot of Inertial Navigation Test Table for fiber optic gyro calibration with three-axis structure
  • Inertial Navigation Test Table shown with full frame design for motion simulation and sensor testing
  • Close-up of Inertial Navigation Test Table high-precision bearing assembly for smooth rotation
  • Inertial Navigation Test Table operating in aerospace lab for UAV inertial sensor calibration
  • Side view of Inertial Navigation Test Table showing compact 60 cm width suitable for labs

Inertial Navigation Test Table for fiber optic gyro and motion sensor calibration in UAV and aerospace applications

No.HY-INS3-550CB
The Inertial Navigation Test Table is a precision motion simulator designed for gyroscope testing, MEMS sensor verification, and INS calibration. It delivers 3 arc seconds accuracy, supports up to 60 kg payload, and offers three-axis dynamic control for stable performance. Widely applied in UAV navigation validation, autonomous vehicle IMU calibration, and satellite payload alignment, it ensures reliable measurement for industrial R&D and marine navigation systems.
Specifications
Load weight:
60KG
Accuracy:
≤±3 arc sec
Range:
±0.001~500deg/sec
Acceleration(with load):
500 deg/sec2
Temperature range:
≥〔-50℃~+70℃〕
Download
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  • White background shot of Inertial Navigation Test Table for fiber optic gyro calibration with three-axis structure
  • Inertial Navigation Test Table shown with full frame design for motion simulation and sensor testing
  • Close-up of Inertial Navigation Test Table high-precision bearing assembly for smooth rotation
  • Inertial Navigation Test Table operating in aerospace lab for UAV inertial sensor calibration
  • Side view of Inertial Navigation Test Table showing compact 60 cm width suitable for labs

Description

Unit Under Test (UUT)
Load weight 60KG
Load height less than 500mm
Load table size Φ550mm
Slip rings to UUT Signal 80 ways, 3A @ 380VAC/50Hz,  40KW(Max)
Power 6 ways@220V/10A
Specifications
Inner Axis Middle Axis Outer Axis
Angular freedom continuous continuous continuous
Position
Accuracy ≤±3 arc sec ≤±3 arc sec ≤±3 arc sec
Resolution 0.36 arc sec 0.36 arc sec 0.36 arc sec
Repeatability <2 arc sec <2 arc sec <2 arc sec
Rate
Range ±0.001~500deg/sec ±0.001~200deg/sec ±0.001~100deg/sec
Maximum speed of three-axis linkage ±60deg/sec
Resolution 0.0001 deg/sec
Accuracy and stability When θ<1 deg/sec ≤1×10-3 (1 deg average)
When 1 deg/sec<θ<10 deg/sec ≤1×10-4 (10 deg average);
When θ≥10 deg/sec ≤1×10-5 (360 deg average)
Dynamic
Acceleration(with load) 500 deg/sec2 150 deg/sec2 100 deg/sec2
Mechanical
Wobble ±3 arc sec ±3 arc sec
Orthogonality ±3 arc sec ±3 arc sec
Swing Range 0°~±45 deg 0°~±45 deg 0°~±45 deg
Swing frequency 0.2deg/10Hz 0.2deg/3Hz 0.2deg/3Hz
Temperature Chamber (TC)
Working volume 600*600*600mm
Temperature range ≥〔-50℃~+70℃〕
Temperature stability ≤±1℃
Temperature deviation: ≤±1℃
Temperature change rate ≥2℃/min
Temperature gradient: ≤2℃
Dimensions
Machine platform dimensions 2750*1050*3110mm
Total weight 3000Kg