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107篇 您的检索式：作者名="Balas G J"

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	题名	作者	年代	出处	被引量
1	The use of shape memory alloy for passive structural damping显示文摘	Thomson P Balas G J Ceo P H	1995	Smart Mater Struct1995，4，1：	2
2	Design of nonlinear controllers for active vehicle suspension using parameter-varying control synthesis显示文摘	Fialho J I and Balas J G	2000	Vehicle System Dynamics2000，33，：	1
3	Pseudoelastic hysteresis medels of shape-memory wires and effects on passive structural damping显示文摘	P Thomson Balas G J	1995	SPIE1995，2445，：	1
4	Invariant subspaces for LPV systems and their applications显示文摘	Balas G Bokor J Szab'o Z	2003	IEEE Trans on Automatic Control2003，48，11：	1
5	Longitudinal motion control of a high-speed supercavitation vehicle 显示文摘	VANEK B BOKOR J BALAS G J	2007	Journal of Vibration and Control2007，13，2：	1
6	Road adaptive active suspension design using linear parameter-varying gain-scheduling 显示文摘	Fialhm I Balas G J	2002	IEEE Transactions on Control Systems Technology2002，10，1：	1
7	Receding horizon control of an F-16 aircraft:a comparative study显示文摘	Keviczky T Balas G J	2006	Control Engineering Practice2006，14，9：	1
8	Disparity for the minor histocompatibility antigen HA-1 is associated with an increased risk of acute graft-versus-host disease(GvHD)but it does not affect chronic GvHD incidence,disease-free survival or overall survival after allogeneic human leucocyte antigen-identical sibling donor transplantation显示文摘	Arostegui JI Balas A Torres A Caballero D Carreras E Brunet S Jimenez A Mataix R Serrano D Vallejo C Sanz G Solano C Rodriguez-Luaces M Marin J Baro J Sanz C Roman J Gonzalez M Martorell J Sierra J Martin C de la Camara R Granena A	2001	Br J Haematol2001，114，4：	1
9	Gain- scheduled lateral control of the F-14 aircraft during pow- ered approach landing 显示文摘	FIALHO I BALAS G J PACKARD A K	2000	Journal of Guidance Control and Dynamics2000，23，3：	1
10	Development of linear-parametervarying models for aircraft显示文摘	MARCOS A BALAS G J	2004	Journal of Guidance Control and Dynamics2004，27，2：	1
11	Con- trol of the F-14 aircraft lateral-directional axis during pow- ered approach 显示文摘	BALAS G J PACKARD A K RENFROW J	1998	Journal of Guidance Control and Dy- namics1998，21，6：	1
12	Robust Dynamic Inversion for Control of Highly Maneuverable Aircraft显示文摘	REINER J BALAS G J WILLIAM L G	1995	Journal of Guidance Control and Dynamics1995，18，1：	1
13	Robust dynamic inversion for control of highly maneuverable aircraft显示文摘	Reiner J Balas G J	1995	Journal of Guidance Control and Dynamics1995，18，1：	1
14	Optimal Scaled H∞ Full Information Control Synthesis with Real uncertainty显示文摘	BALAS G J LIND R	1996	Journal of Guidance Control and Dynamics1996，19，4：	1
15	Development of linear-parameter-varying models for aircraft显示文摘	Marcos A Balas G J	2004	Journal of Guidance Control and Dyna- mics2004，27，2：	1
16	Development of Linear - Parameter -Varying Models for Aircraft 显示文摘	Marcos A Balas G J	2004	Journal of Guidance Control and Dynamics2004，27，2：	1
17	Gut-liver axis and sensing microbes显示文摘	Szabo G Bala S Petrasek J	2010	Dig Dis2010，28，6：	1
18	Linear Parameter Varying Detection Filter Design for a Boeing 747-100/200 Aircratt 显示文摘	Szaszi I Marcos A Balas G J Bokor J	2005	Journal of Guidance Control and Dynamics2005，28，3：	1
19	System identification with generalized orthonormal basis functions: an application to flexible structures显示文摘	Nalbantoglu V Bokor J Balas G	2003	Control Engineering Practice2003，11，3：	1
20	Flight Control Design Using Robust Dynamic Inversion and Time-Scale Separation显示文摘	Reiner J Balas G J Garrard W L	1996	Automatica1996，32，11：	1

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