A Decentralized Active Control System for a Large Flexible Structure in Space,

Abstract

A new strategy in controlling the modal shapes of large structure in space is presented in this study. An active low authority modal control system, consisting of a discrete number of servo system units (M.C.U.) distributed along flexible masts supporting RF radiators, is provided to measure and control the local structural deformations in order to obtain a modal shapes resulting in acceptable pointing error for the RF radiators. Each servo unit is conceived as a model following control system implementing a strategy based on FFT(Fast Fourier Transforms) pairs computations. The control efforts applied by the M.C.U.s to the mast control points are made proportional to the spectral error function generated by a real time F.F.T dedicated microprocessor as the difference between the measured and desidered modal spectra relative to the antenna angular deflections in respect to a fixed set point. The decentralized control system organized by a central controller residing in the master M.C.U., will force the antenna to match the model dynamical behaviour which is expected to improve the antenna pointing accuracy within the L.S.S. design requirements. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1984
Accession Number
ADP003397

Entities

People

  • A. Danesi

Organizations

  • Sapienza University of Rome

Tags

DTIC Thesaurus Topics

  • Accuracy
  • Computations
  • Control Systems
  • Deflection
  • Errors
  • Fast Fourier Transforms
  • Flexible Structures
  • Guidance
  • Mathematics
  • Microprocessors
  • Spacecraft
  • Spectra
  • Vehicles

Fields of Study

  • Engineering
  • Physics

Readers

  • Computer Science/Computer Engineering/Data Science/Digital Signal Processing.
  • Electromagnetic Wave Scattering and Antenna Radiation Engineering
  • Structural Dynamics.

Technology Areas

  • Space
  • Space - Spacecraft Maneuvers