Base Motion Isolation of a Two-Axis Beam Deflector

Abstract

The base motion isolation characteristics of an optical deflector with a two-axis gimbal support are investigated. The particular configuration of the beam deflector system considered utilizes rate integrating gyros to provide a rate inner control loop with an optical tracker providing an outer position control loop. Base motion isolation is partially achieved by the gimbal support assumed to be frictionless. However, input beam motion relative to the optical surface of the beam deflector is shown to produce large excursions of the output beam. As a result, a feed-forward control loop is added to measure and compensate for input beam motion, i.e., base motion.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1972
Accession Number
AD0743002

Entities

People

  • Gary C. Comfort

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Air Platforms
  • Sensors
  • Space

DTIC Thesaurus Topics

  • Accelerometers
  • Accuracy
  • Air Force
  • Airborne
  • Aircrafts
  • Angular Momentum
  • Classification
  • Control Systems
  • Elevation
  • Equations
  • Frequency
  • Frequency Response
  • Line Of Sight
  • Measurement
  • Resonant Frequency
  • Security
  • Spectra

Fields of Study

  • Physics

Readers

  • Control Systems Engineering.
  • Optical Physics and Photonics.