Robustness Study of the Dynamic Inversion Based Indirect Adaptive Control of Flight Vehicles with Uncertain Model Data

Abstract

The objective of this paper is to analyze the stability robustness of dynamic inversion based control laws being used for flight control with uncertainties in model data such as the aerodynamic stability and control derivatives. In particular, the proposed method is aimed at determining the robustness of an indirect adaptive control system developed by the researchers at the AFRL, which is built around a baseline dynamic inversion inner loop. MATLAB/SIMULINK is the environment used for the development and simulation of the flight controller.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 2002
Accession Number
ADA410308

Entities

People

  • David B. Doman
  • Praveen Shankar
  • Rama K. Yedavalli

Organizations

  • Ohio State University

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Air Force Research Laboratories
  • Aircrafts
  • Closed Loop Systems
  • Control Surfaces
  • Control Systems
  • Equations
  • Equations Of Motion
  • Inversion
  • Law
  • Military Research
  • Models
  • Nonlinear Systems
  • Space Systems
  • United States
  • Vehicles

Fields of Study

  • Engineering

Readers

  • Computational Modeling and Simulation
  • Control Systems Engineering.