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High-Performance Aerospace Grade Motion Simulator Rate Table for INS Verification 1-Year Warranty

High-Performance Aerospace Grade Motion Simulator Rate Table for INS Verification 1-Year Warranty

MOQ: 1 set
Payment Method: T/T
Detail Information
Place of Origin
Hubei China
Brand Name
Wuhan Deep Pilot
Product Description

Product Overview

This aerospace-grade rate table is designed for high-performance verification and calibration of inertial navigation systems (INS), including gyroscopes, accelerometers, and optical guidance components. It provides ultra-precise angular rate control, smooth operation, and long-term reliability, making it ideal for aviation, marine, and UAV applications.

The system integrates advanced multi-axis motion control with dynamic environmental simulation, enabling accurate trajectory emulation and rigorous operational testing under extreme conditions.

Key Features

  • High-precision 3-axis control

    • Ensures accurate angular rate and positioning

    • Supports complex motion simulation: position, rate, and swing modes

  • High load adaptability

    • Stable performance with varying payloads

  • Wide angular speed range

    • Supports both low-speed calibration and high-speed dynamic simulation

  • High-speed dynamic simulation

    • Enables precise trajectory emulation for aerospace, defense, and marine environments

  • Reliable INS calibration

    • Ideal for gyroscopes, accelerometers, optical guidance systems, and communication antennas

    • Ensures repeatable and stable testing under extreme conditions

Hardware Construction

  • Modular mechanical design for easy maintenance

  • Multiple safety protections for secure operation

  • Real-time monitoring and precise motion control

  • Self-checking and self-calibration for intelligent, stable operation

  • Industrial-grade control computer for high performance and reliability

Software Features (MotorHost Control Software)

  • One-click device identification

  • Accurate and efficient trajectory planning

  • Real-time motion control adjustments

  • Full-function testing infrastructure

  • User-friendly human-machine interface

  • Intelligent early warning and fault handling system

1. Load Installation
- Dimensions (min) 400 mm (L) × 400 mm (W) × 350 mm (H)
- Mass Range (incl. fixtures) 1 kg ~ 40 kg
- Max Load Inertia 0.4 kg•m²
2. Structural Requirements
- Rotation Angle Continuous infinite rotation
- Structure Type UOO
- Three-Axis Perpendicularity ≤ ±2 arcsec
- Three-Axis Intersection ≤ Ø0.5 mm sphere
- Inner Frame Mounting Surface Flatness ≤ 0.02 mm
- Axis Tilt Rotation Accuracy ±2 arcsec
- Reference Prism (North Guidance) Mounting accuracy ≤ ±5 arcsec
- Locking Mechanism Middle frame: Mechanical lock
Inner/Middle/Outer axes: Electromagnetic locks
- Horizontal Adjustment Range Ensures installation adjustment accuracy ≤ ±2 arcsec
3. Position Indicators
- Angular Position Accuracy ±2 arcsec
- Angular Repeatability ±1 arcsec
- Angular Resolution 0.36 arcsec
4. Angular Velocity
- Range:
  Outer Axis ±0.001°/s ~ ±500°/s
  Middle Axis ±0.001°/s ~ ±600°/s
  Inner Axis ±0.001°/s ~ ±1000°/s
  Max 3-Axis Linkage ±60°/s
- Accuracy:
  ω ≥ 10°/s 0.00001 (360° avg)
  1°/s ≤ ω < 10°/s 0.0001 (10° avg)
  ω < 1°/s 0.001 (1° avg)
- Stability:
  ω ≥ 10°/s 0.00001 (360° avg)
  1°/s ≤ ω < 10°/s 0.0001 (10° avg)
  ω < 1°/s 0.001 (1° avg)
5. Max Angular Acceleration
- Outer Axis (with load) 100°/s²
- Middle Axis (with load) 200°/s²
- Inner Axis (with load) 300°/s²
6. Swing Function
- Formula a=A(2πf)2a=A(2πf)2
Where: a = acceleration, A = amplitude, f = frequency
- Swing Frequencies 6 Hz, 8 Hz, 10 Hz (limited by max acceleration)


products
PRODUCTS DETAILS
High-Performance Aerospace Grade Motion Simulator Rate Table for INS Verification 1-Year Warranty
MOQ: 1 set
Payment Method: T/T
Detail Information
Place of Origin
Hubei China
Brand Name
Wuhan Deep Pilot
Minimum Order Quantity:
1 set
Payment Terms:
T/T
Product Description

Product Overview

This aerospace-grade rate table is designed for high-performance verification and calibration of inertial navigation systems (INS), including gyroscopes, accelerometers, and optical guidance components. It provides ultra-precise angular rate control, smooth operation, and long-term reliability, making it ideal for aviation, marine, and UAV applications.

The system integrates advanced multi-axis motion control with dynamic environmental simulation, enabling accurate trajectory emulation and rigorous operational testing under extreme conditions.

Key Features

  • High-precision 3-axis control

    • Ensures accurate angular rate and positioning

    • Supports complex motion simulation: position, rate, and swing modes

  • High load adaptability

    • Stable performance with varying payloads

  • Wide angular speed range

    • Supports both low-speed calibration and high-speed dynamic simulation

  • High-speed dynamic simulation

    • Enables precise trajectory emulation for aerospace, defense, and marine environments

  • Reliable INS calibration

    • Ideal for gyroscopes, accelerometers, optical guidance systems, and communication antennas

    • Ensures repeatable and stable testing under extreme conditions

Hardware Construction

  • Modular mechanical design for easy maintenance

  • Multiple safety protections for secure operation

  • Real-time monitoring and precise motion control

  • Self-checking and self-calibration for intelligent, stable operation

  • Industrial-grade control computer for high performance and reliability

Software Features (MotorHost Control Software)

  • One-click device identification

  • Accurate and efficient trajectory planning

  • Real-time motion control adjustments

  • Full-function testing infrastructure

  • User-friendly human-machine interface

  • Intelligent early warning and fault handling system

1. Load Installation
- Dimensions (min) 400 mm (L) × 400 mm (W) × 350 mm (H)
- Mass Range (incl. fixtures) 1 kg ~ 40 kg
- Max Load Inertia 0.4 kg•m²
2. Structural Requirements
- Rotation Angle Continuous infinite rotation
- Structure Type UOO
- Three-Axis Perpendicularity ≤ ±2 arcsec
- Three-Axis Intersection ≤ Ø0.5 mm sphere
- Inner Frame Mounting Surface Flatness ≤ 0.02 mm
- Axis Tilt Rotation Accuracy ±2 arcsec
- Reference Prism (North Guidance) Mounting accuracy ≤ ±5 arcsec
- Locking Mechanism Middle frame: Mechanical lock
Inner/Middle/Outer axes: Electromagnetic locks
- Horizontal Adjustment Range Ensures installation adjustment accuracy ≤ ±2 arcsec
3. Position Indicators
- Angular Position Accuracy ±2 arcsec
- Angular Repeatability ±1 arcsec
- Angular Resolution 0.36 arcsec
4. Angular Velocity
- Range:
  Outer Axis ±0.001°/s ~ ±500°/s
  Middle Axis ±0.001°/s ~ ±600°/s
  Inner Axis ±0.001°/s ~ ±1000°/s
  Max 3-Axis Linkage ±60°/s
- Accuracy:
  ω ≥ 10°/s 0.00001 (360° avg)
  1°/s ≤ ω < 10°/s 0.0001 (10° avg)
  ω < 1°/s 0.001 (1° avg)
- Stability:
  ω ≥ 10°/s 0.00001 (360° avg)
  1°/s ≤ ω < 10°/s 0.0001 (10° avg)
  ω < 1°/s 0.001 (1° avg)
5. Max Angular Acceleration
- Outer Axis (with load) 100°/s²
- Middle Axis (with load) 200°/s²
- Inner Axis (with load) 300°/s²
6. Swing Function
- Formula a=A(2πf)2a=A(2πf)2
Where: a = acceleration, A = amplitude, f = frequency
- Swing Frequencies 6 Hz, 8 Hz, 10 Hz (limited by max acceleration)