Design of robust autopilot-output integral sliding mode controllers for guided missile systems with parameter perturbations

Author： Jafarov Elbrous M   Tasaltin Ramazan  

Publisher： Emerald Group Publishing Ltd

ISSN： 0002-2667

Source： Aircraft Engineering, Vol.73, Iss.1, 2001-02, pp. : 16-26

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

Robust LPV autopilot design for hypersonic reentry vehicle

By  

Aircraft Engineering, Vol. 86, Iss. 5, 2014-08 ,pp. : 423-431

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Simple autopilot design procedure based on a factorization approach

By Nassirharand Amir   Alizadeh Mohammad Hosain  

Aircraft Engineering, Vol. 78, Iss. 5, 2006-09 ,pp. : 407-414

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

The N.A.C.A.'s Role in Guided Missile Research

By Shortal Joseph A.  

Aircraft Engineering, Vol. 25, Iss. 4, 1993-12 ,pp. : 96-100

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Frequency-Domain Sliding Mode Design Technique Applied to the Control of a Ducted Fan Micro-Air Vehicle

By Hess R. A.   Ussery T. M.  

Journal of the American Helicopter Society, Vol. 49, Iss. 4, 2004-10 ,pp. : 457-467

AHS International

Access to resources Recommend Favorite

Robust stabilization of input-delayed systems with design example for rocket motor control

By Jafarov Elbrous M.  

Aircraft Engineering, Vol. 80, Iss. 1, 2008-01 ,pp. : 59-65

Emerald Group Publishing Ltd

Access to resources Recommend Favorite