ePrints@IIScePrints@IISc Home | About | Browse | Latest Additions | Advanced Search | Contact | Help

Robustness Study of a Dynamic Inversion Control Law for a High Performance Aircraft

Tripathi, Abha and Padhi, Radhakant (2008) Robustness Study of a Dynamic Inversion Control Law for a High Performance Aircraft. In: Proceedings of the International Conference on Aerospace Science and Technology, 26-28 June 2008, Bangalore, India.

[img] PDF
Robustness.pdf - Published Version
Restricted to Registered users only

Download (188Kb) | Request a copy

Abstract

In the design of °ight control system modeling uncertainties in the form of param-eter variations is one of the major problems. It is even more critical for high performance aircrafts,since such aircrafts are purposefully designed unstable to enhance their performance (especially ma-neuverability). Hence the °ight control system needs to be quite e®ective in both assuring accurate tracking of pilot commands, while simultaneously assuring overall stability of the aircraft. In addi-tion, the control system must also be su±ciently robust to cater for possible parameter variations and inaccuracies . The primary aim of this paper is to carry out a robustness study of a dynamic inversion based nonlinear control design for a high performance aircraft, which has been developed recently [1].

Item Type: Conference Paper
Department/Centre: Division of Mechanical Sciences > Aerospace Engineering (Formerly, Aeronautical Engineering)
Date Deposited: 29 Sep 2011 05:03
Last Modified: 29 Sep 2011 05:03
URI: http://eprints.iisc.ernet.in/id/eprint/40980

Actions (login required)

View Item View Item