Accession Number:

ADA411945

Title:

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

Descriptive Note:

Conference paper

Corporate Author:

OHIO STATE UNIV COLUMBUS

Report Date:

2003-02-01

Pagination or Media Count:

18.0

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.

Subject Categories:

  • Flight Control and Instrumentation

Distribution Statement:

APPROVED FOR PUBLIC RELEASE