A Second Generation of Backstepping Designs and Robust Nonlinear Control of Aeroengines

Abstract

The objective of this research has been twofold: (1) to develop nonlinear control design techniques that can systematically accommodate nonlinearities and have optimality properties, and (2) develop control methods for robust stabilization and optimization of performance of aeroengine compressor systems.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1997
Accession Number
ADA356727

Entities

People

  • Miroslav Krstić

Organizations

  • University of Maryland

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Air Force
  • Aircraft Wings
  • Aircrafts
  • Compressors
  • Demographic Cohorts
  • Engineering
  • Equations
  • Feedback
  • Information Science
  • Jet Engines
  • Law
  • Linear Systems
  • Mechanical Engineering
  • Nonlinear Systems
  • Students
  • Universities
  • Word Processors

Readers

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