• Dual-axis motion simulator for aerospace and high-reliability testing on white background
  • Motion test stand with high load capacity for flight control component validation
  • Close up of precision encoder ensuring accurate angle measurement for gyro calibration
  • Motion simulator performing attitude simulation for satellite component testing
  • Test equipment dimensions on aerospace workbench with heavy duty support
  • Automated control interface executing guidance system calibration sequence
  • Dual-axis motion simulator for aerospace and high-reliability testing on white background
  • Motion test stand with high load capacity for flight control component validation
  • Close up of precision encoder ensuring accurate angle measurement for gyro calibration
  • Motion simulator performing attitude simulation for satellite component testing
  • Test equipment dimensions on aerospace workbench with heavy duty support
  • Automated control interface executing guidance system calibration sequence

Dual Axis Motion Simulator for Aerospace and High-Reliability Testing

No.BE-INS2-23C01
This dual-axis motion simulator serves as gyroscope test stand and inertial navigation test table for high-reliability aerospace and mission-critical applications. It combines exceptional angle measurement accuracy with rapid dynamic response and minimal overshoot, ensuring precise attitude control simulation. Supporting 40kg payload with wide heading and pitch ranges, it enables flight control validation,satellite component testing, and guidance system calibration in demanding R&D environments.
Specifications
Load weight:
≥40kg
Angle measurement accuracy:
≤0.005°
Heading angle range:
±45°
Maximum angular acceleration:
≥40°/s²
Rate accuracy:
≤0.01°
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  • Dual-axis motion simulator for aerospace and high-reliability testing on white background
  • Motion test stand with high load capacity for flight control component validation
  • Close up of precision encoder ensuring accurate angle measurement for gyro calibration
  • Motion simulator performing attitude simulation for satellite component testing
  • Test equipment dimensions on aerospace workbench with heavy duty support
  • Automated control interface executing guidance system calibration sequence

Description

Technical Specifications

Parameter

Specification

Dynamic performance

0.2°@2Hz

Angle measurement accuracy

≤0.005°

Step response overshoot

≤10%

Heading angle range

±45°

Pitch angle range

-15°~+45°

Minimum angular velocity

≤0.005°/s

Maximum angular velocity

≥4°/s

Maximum angular acceleration

≥40°/s²

Rate accuracy

≤0.01° (1σ)

Load weight

≥40kg