Robust identification method for nonlinear model structures and its application to high-performance aircraft

ISSN： 1464-5319

Source： International Journal of Systems Science, Vol.44, Iss.6, 2013-06, pp. : 1040-1051

Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.

Previous Menu Next

Abstract

Related content

Application of the weight function method on a high incidence research aircraft model

The Aeronautical Journal, Vol. 117, Iss. 1195, 2013-09 ,pp. : 897-912

Cambridge University Press

Access to resources Recommend Favorite

A robust algorithm for model-following control of under-actuated systems, and its application to a non-holonomic robot and an aircraft

By Han Youngmo

International Journal of Systems Science, Vol. 36, Iss. 6, 2005-05 ,pp. : 341-356

Taylor & Francis Ltd

Access to resources Recommend Favorite

Nonlinear identification and control of aircraft

By Lyshevski Sergey Edward

International Journal of Systems Science, Vol. 31, Iss. 8, 2000-08 ,pp. : 923-935

Taylor & Francis Ltd

Access to resources Recommend Favorite

The adjoint method coupled with the modal identification method for nonlinear model reduction

By Favennec Y. Girault§ M. Petit D.

Inverse Problems in Science and Engineering, Vol. 14, Iss. 2, 2006-03 ,pp. : 153-170

Taylor & Francis Ltd

Access to resources Recommend Favorite

Neural-fuzzy scheduling of H robust controllers for a high performance fighter aircraft under a Herbst-like manoeuvre

By Wang Jianliang Zhang Weiqiang

International Journal of Control, Vol. 72, Iss. 7-8, 1999-05 ,pp. : 740-754

Taylor & Francis Ltd

Access to resources Recommend Favorite