Robust Adaptive Control and Its Applications to Missile Autopilots

Abstract

This final report summarizes the achievements of our research program, and describes the research results obtained during the past three years. Our work has focused on Air Force application platforms of compressor control, and design of missile autopilot. Several results were obtained in the past three years. The first one was local feedback control laws that stabilize the critical operating condition of the axial flow compression system governed by Moore-Greitzer model. The second one was missile autopilot design with time-varying control techniques where time-varying spectrum theory was used. The last one was the simulation study for feedback stabilization of compression control systems by software programming in Simulink Toolbox. In the past three years, the funding for this proposal was able to support Phillip Martin to complete his Master degree, and Michael Mickle to complete most part of his Ph.D Dissertation. Their work produced two journal publications and three conference papers. Therefore our goals for this program were mostly accomplished.

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Document Details

Document Type
Technical Report
Publication Date
Aug 30, 1998
Accession Number
ADA359330

Entities

People

  • Guoxiang Gu

Organizations

  • Louisiana State University

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Automatic Pilots
  • Axial Flow
  • Axial Flow Compressors
  • Closed Loop Systems
  • Compression
  • Compressors
  • Control Systems
  • Electrical Engineering
  • Engineering
  • Feedback
  • Flight Control Systems
  • Flow
  • Signal Processing
  • Simulations
  • Students

Readers

  • Inertial Navigation Systems.
  • Software Engineering.
  • Technical Research and Report Writing.