• Dynamic dual axis rate table for aerospace attitude control gyro testing
  • Motion simulation table with -32° to 32° heading range and 3Hz bandwidth
  • Close up of drive motor for 300 deg per second squared pitch acceleration
  • Rate table performing 3Hz sinusoidal swing for aircraft attitude simulation
  • Automated interface executing high frequency test sequence for gyro validation
  • Dynamic dual axis rate table for aerospace attitude control gyro testing
  • Motion simulation table with -32° to 32° heading range and 3Hz bandwidth
  • Close up of drive motor for 300 deg per second squared pitch acceleration
  • Rate table performing 3Hz sinusoidal swing for aircraft attitude simulation
  • Automated interface executing high frequency test sequence for gyro validation

Dynamic Dual Axis Rate Table for Aerospace Attitude Control Testing

No.BE-INS2-23C10
This dynamic dual axis rate table serves as gyroscope test stand for aerospace attitude control systems. Benefits: 300°/s² pitch angular acceleration enables high frequency swing tests, 3Hz bandwidth supports real-time attitude simulation, and system accuracy at 0.01° after compensation ensures precise gyro validation.
Specifications
Heading movement range:
-32°~32°
Pitch movement range:
-62°~22°
Position accuracy:
0.01°
Maximum angular velocity:
*20°/s
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  • Dynamic dual axis rate table for aerospace attitude control gyro testing
  • Motion simulation table with -32° to 32° heading range and 3Hz bandwidth
  • Close up of drive motor for 300 deg per second squared pitch acceleration
  • Rate table performing 3Hz sinusoidal swing for aircraft attitude simulation
  • Automated interface executing high frequency test sequence for gyro validation

Description

Technical Parameters Description
Corner range Heading movement range: -32°~32°
Pitch movement range: -62°~22°
Maximum acceleration Pitch 200°/s², heading 200°/s²;
The maximum angular acceleration of pitch is 300°/s² for sinusoidal swing function.
At a swing frequency of 3Hz, the amplitude is not less than 0.845°, at a swing frequency of 1Hz, the amplitude is not less than 7.6°, and the search speed is >10°/s;
The maximum angular acceleration of the heading is 250°/s² for sinusoidal swing function. At a swing frequency of 3Hz, the amplitude is not less than 0.7°.
At a swing frequency of 1Hz, the amplitude is not less than 6.3°, and the search speed is >10°/s;
Position accuracy The error is not greater than 0.05°, and the system accuracy after compensation is +36° (0.01°);
Minimum angular velocity (linkage conditions): pitch 0.03°/s; heading 0.03°/s;
Maximum angular velocity *20°/s
Bandwidth Heading is not less than 3Hz;
The pitch is not less than 3Hz.