Control of a nonlinear hybrid system arising in flexible spacecraft

ISSN： 1464-5319

Source： International Journal of Systems Science, Vol.30, Iss.6, 1999-06, pp. : 635-642

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

Integrated nonlinear optimal control of spacecraft in proximity operations

By Xin Ming Pan Hejia

International Journal of Control, Vol. 83, Iss. 2, 2010-02 ,pp. : 347-363

Taylor & Francis Ltd

Access to resources Recommend Favorite

Control of a non-linear PDE system arising from non-burning tokamak plasma transport dynamics

By Schuster Eugenio Krstić Miroslav

International Journal of Control, Vol. 76, Iss. 11, 2003-01 ,pp. : 1116-1124

Taylor & Francis Ltd

Access to resources Recommend Favorite

Velocity-free fault-tolerant control allocation for flexible spacecraft with redundant thrusters

International Journal of Systems Science, Vol. 46, Iss. 6, 2015-04 ,pp. : 976-992

Taylor & Francis Ltd

Access to resources Recommend Favorite

Adaptive fault tolerant control using integral sliding mode strategy with application to flexible spacecraft

By Hu Qinglei Xiao Bing

International Journal of Systems Science, Vol. 44, Iss. 12, 2013-12 ,pp. : 2273-2286

Taylor & Francis Ltd

Access to resources Recommend Favorite

On the exponential stability of an initial-boundary equation arising from strain feedback control of flexible robot arms with rigid offset

By Guo Bao-Zhu Luo Zheng-Hua

International Journal of Control, Vol. 69, Iss. 2, 1998-01 ,pp. : 227-238

Taylor & Francis Ltd

Access to resources Recommend Favorite