Open AccessSub-optimal Autopilot Design based on Dynamic Neural Unit Network for Tactical Missile
Author(s) -
Netra Singh
Publication year - 2016
Publication title -
indian journal of science and technology
Language(s) - English
Resource type - Journals
eISSN - 0974-6846
pISSN - 0974-5645
DOI - 10.17485/ijst/2016/v9is1/107903
Subject(s) - autopilot , control theory (sociology) , missile , computer science , angle of attack , optimal control , artificial neural network , missile guidance , aerodynamics , control engineering , aerospace engineering , mathematics , control (management) , engineering , mathematical optimization , artificial intelligence