Inertial Navigation Test Table for Precision Fiber Optic Gyroscope and IMU Calibration in UAV Aerospace Applications

No.HY-INS3-550CR

This Inertial Navigation Test Table is a high-precision motion simulator designed for gyroscope testing, MEMS sensor verification, and INS calibration. Offering 3 arc seconds accuracy, 60 kg payload, and three-axis dynamic control, it ensures reliability for aerospace, autonomous vehicles, and industrial R&D. It provides stable solutions for fiber optic gyro evaluation and navigation accuracy validation.

Specifications

Load weight:

60KG

Resolution:

0.0001 deg/sec

Acceleration(with load):

500 deg/sec2

Swing Range:

0°～±45 deg

Repeatability:

<2 arc sec

GET A QUOTE

Download

View all downloads

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	600600600mm
Temperature range	≥〔-50℃～+70℃〕
Temperature stability	≤±1℃
Temperature deviation:	≤±1℃
Temperature change rate	≥2℃/min
Temperature gradient:	≤2℃
Dimensions
Machine platform dimensions	275010503110mm
Total weight	3000Kg

Company: About Us

Contact Us: Wuhan. Hubei.China; info@blueequator-ins.com; +86 19571725877

Newsletter: Lorem ipsum dolor si consectetur adipisicing elit, sed eiusmotempor incididunt ut labore et

Follow Us

Inertial Navigation Test Table for Precision Fiber Optic Gyroscope and IMU Calibration in UAV Aerospace Applications

Description