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Design and Testing of a Simulator for Micro-Vibration Testing of Star Sensor.

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A novel six-dimensional micro-vibration simulator accurately replicates space acceleration for star sensors. This Gough-Stewart platform-based system offers high precision and a wide bandwidth, crucial for testing sensitive aerospace components.

Keywords:
acceleration simulatorgravity unloading systemspace micro-vibrationstar sensor

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Area of Science:

  • Aerospace Engineering
  • Mechanical Engineering
  • Vibration Analysis

Background:

  • Spacecraft components, like star sensors, face micro-vibration environments.
  • Accurate simulation of these vibrations is critical for mission success.
  • Existing simulation methods may lack multi-dimensional capabilities.

Purpose of the Study:

  • To design and validate a multi-dimensional micro-vibration simulator.
  • To enable effective reproduction of space six-dimensional acceleration.
  • To assess the performance of the simulator for star sensor applications.

Main Methods:

  • Integrated design of a gravity unloading system and a Gough-Stewart platform-based simulator.
  • Modal analysis to determine natural frequencies and mode shapes.
  • Dynamic equation establishment and co-simulation verification.
  • Whole machine testing using frequency response functions.

Main Results:

  • The simulator successfully reproduces space six-dimensional acceleration.
  • Achieved an output bandwidth of 5-300 Hz.
  • Maximum error in acceleration reproduction was 9.19%.

Conclusions:

  • The micro-vibration simulator offers high precision and a large analog bandwidth.
  • Its compact design facilitates transportation and integration.
  • The platform accurately simulates six-degree-of-freedom space micro-vibrations for star sensors.