Placing all closed loop poles of missile attitude control systems in the sliding mode via the root locus technique

By Huang Y.J.   Way H.K.  

ISA Transactions, Vol. 40, Iss. 4, 2001-09 ,pp. : 333-340

Elsevier

Access to resources Recommend Favorite

Flight Attitude Sliding Mode Control Design Based on the Compensation of Extended State Observer

By  

Applied Mechanics and Materials, Vol. 2014, Iss. 716, 2015-02 ,pp. : 1689-1693

Trans Tech Publications

Access to resources Recommend Favorite

Fault Diagnosis and Fault-Tolerant Control of Micro-Satellite Propulsion Mode Attitude Control

By  

Applied Mechanics and Materials, Vol. 2015, Iss. 764, 2015-06 ,pp. : 607-612

Trans Tech Publications

Access to resources Recommend Favorite

Research on Terminal Piecewise Sliding Mode for Excitation Control System Based on the Nonlinear Disturbance Observer

By  

Applied Mechanics and Materials, Vol. 2014, Iss. 711, 2015-02 ,pp. : 297-302

Trans Tech Publications

Access to resources Recommend Favorite

Adaptive Fuzzy Sliding-Mode Position Control of a Shape Memory Alloy Actuated System

By  

Applied Mechanics and Materials, Vol. 2015, Iss. 789, 2015-10 ,pp. : 946-950

Trans Tech Publications

Access to resources Recommend Favorite