z-logo
open-access-imgOpen Access
Adaptive Control Based on a Parametric Affine Model for Tail-Controlled Missiles
Publication year - 2003
Publication title -
journal of control automation and systems engineering
Language(s) - English
Resource type - Journals
ISSN - 1225-9845
DOI - 10.5302/j.icros.2003.9.7.547
Subject(s) - missile , control theory (sociology) , parametric statistics , adaptive control , affine transformation , computer science , sliding mode control , missile guidance , control engineering , engineering , control (management) , nonlinear system , mathematics , artificial intelligence , physics , aerospace engineering , statistics , pure mathematics , quantum mechanics

The content you want is available to Zendy users.

Already have an account? Click here to sign in.
Having issues? You can contact us here
Accelerating Research

Address

John Eccles House
Robert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom