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

Optimal control for the rolling pullout maneuver of a modern fighter aircraft

Satyanarayana, G and Sarma, IG and Prasad, UR (2007) Optimal control for the rolling pullout maneuver of a modern fighter aircraft. In: 1975 IEEE Conference on Decision and Control including the 14th Symposium on Adaptive Processes, Dec. 1975.

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

Download (145Kb) | Request a copy
Official URL: http://ieeexplore.ieee.org/xpls/abs_all.jsp?arnumb...

Abstract

Optimal control laws are obtained for the elevator and the ailerons for a modern fighter aircraft in a rolling pullout maneuver. The problem is solved for three flight conditions using the conjugate gradient method.

Item Type: Conference Paper
Additional Information: Copyright 2007 IEEE. Personal use of this material is permitted. However, permission to reprint/republish this material for advertising or promotional purposes or for creating new collective works for resale or redistribution to servers or lists, or to reuse any copyrighted component of this work in other works must be obtained from the IEEE.
Department/Centre: Division of Mechanical Sciences > Aerospace Engineering (Formerly, Aeronautical Engineering)
Date Deposited: 27 Dec 2011 08:28
Last Modified: 27 Dec 2011 08:28
URI: http://eprints.iisc.ernet.in/id/eprint/42911

Actions (login required)

View Item View Item