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检索条件"主题词=Predictive Control Method"
25 条 记 录,以下是21-30 订阅
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Optimal control Framework for a Centralized Approach to Separation Management
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JOURNAL OF GUIDANCE control AND DYNAMICS 2014年 第3期37卷 1033-1038页
作者: Walter, Leif Kostina, Ekaterina French German Inst St Louis F-68301 St Louis France Univ Marburg Fac Math & Comp Sci D-52425 Marburg Germany
I. Introduction With the increase in demand and capacity, Air Traffic Management (ATM) will face further challenges to keep delay considerably low while increasing safety standards at a cheaper cost. When addressing t... 详细信息
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Robust Generalized predictive control with Uncertainty Quantification
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JOURNAL OF GUIDANCE control AND DYNAMICS 2012年 第3期35卷 930-937页
作者: Lew, Jiann-Shiun Juang, Jer-Nan Tennessee State Univ Ctr Excellence Informat Syst Nashville TN 37209 USA Natl Cheng Kung Univ Tainan 70101 Taiwan
This paper presents a robust predictive control method with uncertainty quantification for problems, such as online aircraft flutter suppression. The proposed approach begins by identifying the multistep output predic... 详细信息
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Software-enabled receding horizon control for autonomous unmanned aerial vehicle guidance
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JOURNAL OF GUIDANCE control AND DYNAMICS 2006年 第3期29卷 680-694页
作者: Keviczky, Tamas Balas, Gary J. Univ Minnesota Control Sci & Dynam Syst Ctr Minneapolis MN 55455 USA Univ Minnesota Dept Aerosp Engn & Mech Minneapolis MN 55455 USA
This paper describes autonomous unmanned aerial vehicle (UAV) guidance technologies developed and demonstrated in a flight test sponsored by the DARPA Software Enabled control program. The flight experiment took place... 详细信息
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Four-dimensional guidance of atmospheric vehicles
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JOURNAL OF GUIDANCE control AND DYNAMICS 1996年 第1期19卷 113-122页
作者: StiharuAlexe, I OShea, J POLYTECH UNIV BUCHARESTROMANIA
The nonlinear control theories based upon the model predictive control and the nonlinear inverse control are used to develop four-dimensional guidance controllers, the conversion of the primary trajectory being assume... 详细信息
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AIRCRAFT TERRAIN FOLLOWING BASED ON A NONLINEAR CONTINUOUS predictive control APPROACH
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JOURNAL OF GUIDANCE control AND DYNAMICS 1995年 第4期18卷 817-823页
作者: LU, P PIERSON, BL Iowa State University Ames Iowa 50011-3231
This paper discusses aircraft terrain-following flight control law development based on a new nonlinear optimal predictive control method, The control law minimizes the predicted difference between the actual trajecto... 详细信息
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