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31
High-Gain Estimator and Fault-Tolerant Design With Application to a Gas Turbine Dynamic System.
High-Gain Estimator and Fault-Tolerant Design With Application to a Gas Turbine Dynamic System.
Zhiwei Gao, | Institute of Electrical and Electronics Engineers | 2007 ,
32
Distributed Robust Receding Horizon Control for Multivehicle Guidance.
Distributed Robust Receding Horizon Control for Multivehicle Guidance.
Yoshiaki Kuwata, | Institute of Electrical and Electronics Engineers | 2007 ,
33
Stabilization of a PVTOL Aircraft and an Inertia Wheel Pendulum Using Saturation Technique.
Stabilization of a PVTOL Aircraft and an Inertia Wheel Pendulum Using Saturation Technique.
Huawen Ye, | Institute of Electrical and Electronics Engineers | 2007 ,
34
Disturbance-rejection high-precision motion control of a Stewart platform
Disturbance-rejection high-precision motion control of a Stewart platform
Yu Xin Su, | Institute of Electrical and Electronics Engineers | 2004 ,
35
Observing a three-tank system
Observing a three-tank system
Ming Hou, | Institute of Electrical and Electronics Engineers | 2005 ,
36
Constrained H∞ control of active suspensions: an LMI approach
Constrained H∞ control of active suspensions: an LMI approach
Hong Chen, | Institute of Electrical and Electronics Engineers | 2005 ,
37
Identification of nonlinear systems using generalized kernel models
Identification of nonlinear systems using generalized kernel models
Sheng Chen, | Institute of Electrical and Electronics Engineers | 2005 ,
38
A variable structure multirate State estimator for seeking control of HDDs
A variable structure multirate State estimator for seeking control of HDDs
Keitaro Ohno, | Institute of Electrical and Electronics Engineers | 2005 ,
39
Experimental results on adaptive output feedback control using a laboratory model helicopter
Experimental results on adaptive output feedback control using a laboratory model helicopter
Ali T. Kutay, | Institute of Electrical and Electronics Engineers | 2005 ,
40
Modeling and H∞ control for switched linear parameter-varying missile autopilot.
Modeling and H∞ control for switched linear parameter-varying missile autopilot.
Sungyung Lim, | Institute of Electrical and Electronics Engineers | 2003 ,
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