A STUDY IN FINAL-VALUE CONTROL,

Abstract

The difficulty encountered in operating a final-value control system in a closed-loop configuration is that the feedback gains become infinite at the final time and thus are impossible to implement. This thesis examines several alternative configurations to the closed-loop system for the Titan III booster using Flight Plan I pitch steering. (Author)

Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1970
Accession Number
AD0708152

Entities

People

  • Marlin Clarence Leiding

Organizations

  • University of California, Los Angeles

Tags

DTIC Thesaurus Topics

  • Closed Loop Systems
  • Control Surfaces
  • Control Systems
  • Feedback
  • Guide Vanes
  • Steering

Readers

  • Control Systems Engineering.
  • Rocket Propulsion.
  • Systems Analysis and Design