Control of a Spinning Projectile,

Abstract

Powerful multivariable robust control synthesis techniques which have recently been devised (1) are applied to a tracking problem for a spinning projectile. A linearized lateral axis model of the projectile is used to design a reduced order LQG compensator to command angle of attack and sideslip using only fixed plane pitch rate and yaw rate measurements. Singular values of various transfer function matrices are used to explain the design procedure to obtain robust compensation that recovers the full state feedback guaranteed gain and phase margins. (Author)

Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1982
Accession Number
ADP001092

Entities

People

  • J. E. Wall Jr
  • N. A. Lehtomaki

Organizations

  • Honeywell International, Inc.

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Attitude (Inclination)
  • Compensation
  • Compensators
  • Control Theory
  • Feedback
  • Measurement
  • Michigan
  • Orientation (Direction)
  • Projectiles
  • Sideslip
  • Transfer Functions
  • Yaw

Readers

  • Adaptive Control and Estimation with Uncertainty in Dynamic Systems.
  • Control Systems Engineering.