Combining State Dependent Riccati Equation Approach With Dynamic Inversion: Application to Control of Flight Vehicles

Abstract

State Dependent Algebraic Riccati Equation (SDRE) techniques are rapidly emerging as a design method, which provides a systematic and effective means of designing nonlinear controllers, observers, and filters. This paper describes a new method of integrating the SDRE technique with the Dynamic Inversion control law that is frequently used in the design of aircraft control systems. This paper also provides an example by applying this control design technique to a reusable launch vehicle.

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 2003
Accession Number
ADA411945

Entities

People

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

Organizations

  • Ohio State University

Tags

Communities of Interest

  • Counter WMD
  • Space

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Air Force Research Laboratories
  • Aircrafts
  • Closed Loop Systems
  • Control Systems
  • Equations
  • Inversion
  • Launch Vehicles
  • Law
  • Military Research
  • Nonlinear Systems
  • Reusable Launch Vehicles
  • Riccati Equation
  • United States
  • Vehicles

Fields of Study

  • Engineering

Readers

  • Adaptive Control and Estimation with Uncertainty in Dynamic Systems.
  • Robotics and Automation.