Towards Overexpression of the Serotonin Transporter - An Overview

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[唯一标识符]:CDSTIC.ISTP.1611383
[文献来源]:科学技术会议录索引(ISTP)
[文献类型]:科技会议
[标题]:Towards Overexpression of the Serotonin Transporter - An Overview
[作者]:FM Titgemeyer;P Schloss;CR Baker;DC Williams;S Hilbererehret;AK Boer;GT Robillard
[出版单位]:Plenum Press Div Plenum Publishing CorpNew York
[ISSN_ISBN]:0-306-45705-9
[会议名称]:11th Meeting of the European-Society-for-Neurochemistry,Groningen, Netherlands,June 15-20, 1996
[来源]:NEUROCHEMISTRY - CELLULAR, MOLECULAR, AND CLINICAL ASPECTS,pp 773-781
[编辑者]:EA Teelken;J Korf
[主办单位]:European Soc Neurochem
[地址]:FM Titgemeyer,Univ_Groningen, Dept Biochem, Nijenborgh 4, NL-9747 Ag Groningen, Netherlands
[专业领域]:Neurosciences,Clinical Neurology
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[文献类型]:科技报告
[标题]:Special Forces Capabilities of the European Union Military Forces.
[作者]:R. Modigs;
[机构]:Army Command and General Staff Coll., Fort Leavenworth, KS. School of Advanced Military Studies.
[关键词]:military requirements,military forces(foreign),military capabilities,special operations forces,european union,task forces, interoperability, case studies,unconventional operations, helsinki headline goals, petersberg tasks
[出版年份]:2005
[报告时间]:26 May 2004,
[页码]:92p
[馆藏索取号]:AD-A429325
[总页数]:92


[唯一标识符]:CDSITC.AEROSPACE.A95-41783
[文献来源]:美国航空航天数据库(aerospace)
[资源原始索取号]:A1995-41783; Reference AN: A95-41783
[标题]:Fuzzy logic in restructurable flight control systems
[作者]:Ho Howard S; Balakrishnan S N
[书名]:IN: 1995 American Control Conference, 14th, Seattle, WA, June 21-23, 1995, Proceedings. Vol. 2 (A95-41649 11-63), Piscataway, NJ, Institute of Electrical and Electronics Engineers, 1995, p. 1362-1366
[文摘]:In this paper, a fuzzy logic controller (FLC) is proposed for restructurable flight control systems. The role of the FLC is to stabilize the aircraft upon a fault occurrence. The FLC derives pitch/roll/yaw controls from a generic knowledge base characterized by 49 if-then rules. A linearized model representative of a modern jet fighter provides the basis for the numerical simulation. Simulated faults include various degrees of surface loss at the right stabilator, combined with reduced ailerons and rudder control power. The FLC accomplishes the stabilization task under test conditions without any knowledge of the system parameters. The numerical results demonstrate the potential of the FLC as a suitable control algorithm that bridges the critical gap between the fault occurrence and the full implementation of the new control law. (Author)
[关键词]:FLIGHT CONTROL; FUZZY SYSTEMS; LOGIC DESIGN; CONTROL SYSTEMS DESIGN; AIRCRAFT STABILITY; AILERONS ; DIGITAL SIMULATION; FLIGHT TESTS
[出版年份]:1995
[专业领域]:AIRCRAFT STABILITY AND CONTROL