By Topic

Robust stability analysis of a lateral flight control system for a missile

Sign In

Cookies must be enabled to login.After enabling cookies , please use refresh or reload or ctrl+f5 on the browser for the login options.

Formats Non-Member Member
$33 $13
Learn how you can qualify for the best price for this item!
Become an IEEE Member or Subscribe to
IEEE Xplore for exclusive pricing!
close button

puzzle piece

IEEE membership options for an individual and IEEE Xplore subscriptions for an organization offer the most affordable access to essential journal articles, conference papers, standards, eBooks, and eLearning courses.

Learn more about:

IEEE membership

IEEE Xplore subscriptions

2 Author(s)
White, B.A. ; Dept. of Aerosp. Power & Sensors, R. Mil. Coll. of Sci., Shrivenham, UK ; Tsourdos, A.

A homing missile lateral autopilot is synthesized by exploiting the fact that under mild differentiability conditions, nonlinear systems can be represented in quasilinear form. The robustness of the lateral missile velocity autopilot to uncertain aerodynamic parameters is then determined using Kharitonov's theorem

Published in:

American Control Conference, 1999. Proceedings of the 1999  (Volume:6 )

Date of Conference: