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上海交通大学自动化系博士研究生乔磊获得2019 IET Control Theory & Applications最佳论文奖（Premium Award）（图）
上海交通大学自动化系 博士研究生 乔磊 2019 最佳论文奖
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2019/12/11
近日收到IET Control Theory & Applications期刊编辑部消息，上海交通大学自动化系博士研究生乔磊及其导师张卫东教授合作的论文‘Lei Qiao, Weidong Zhang, Adaptive non-singular integral terminal sliding mode tracking control for autonomous underwater ve...
Multi-point Wing Planform Optimization via Control Theory
Multi-point Wing Planform Optimization via Control Theory
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2015/7/2
This paper focuses on wing optimization via control theory using a multi-point design method. Based on the design methodology previously developed for wing section and planform optimization at a speci...
OPTIMUM TRANSONIC WING DESIGN USING CONTROL THEORY
OPTIMUM TRANSONIC DESIGN CONTROL THEORY
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2015/7/2
While aerodynamic prediction methods based CFD are now well estab lished, and quite accurate and robust, the ultimate need in the design process is to find the optimum shape which maximizes the ...
Aerodynamic Shape Optimization Techniques Based On Control Theory
Aerodynamic Shape Optimization Techniques Based Control Theory
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2015/7/2
These Lecture Notes review the formulation and application of optimization techniques based on control theory for aerodynamic shape design in both inviscid and viscous compressible ow. The theory is a...
Aerodynamic Shape Optimization Techniques Based On Control Theory
Aerodynamic Shape Optimization Techniques Based Control Theory
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2015/7/2
This paper reviews the formulation and application of optimization techniques based on control theory for aerodynamic shape design in both inviscid and viscous compressible flow. The theory is applied...
Optimum Aerodynamic Design Using CFD and Control Theory
Optimum Aerodynamic Design CFD Control Theory
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2015/7/1
This paper describes the implementation of optimiza-tion techniques based on control theory for airfoil and wing design. The theory is applied to a system de- fined by the partial differential equatio...
Aerodynamic Shape Optimization of Wing and Wing- B CI dy Configurations Using Control Theory
Aerodynamic Shape Optimization Wing- B CI Configurations Control Theory
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2015/7/1
This paper describes the implementation of op-timization techniques based on control theory for wing and wing-body design. In previous stud-ies [18, 19,221 it wasshown that control theory could be use...
Control Theory Based Airfoil Design u for Potential Flow and a Finite Volume Discretization
Control Theory Based Airfoil Design Potential Flow Finite Volume Discretization
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2015/7/1
This paper describes the implementation of opti-mization techniques based on control theory for air-foil design. In previous studies [6, 71 it was shown that control theory could be used to devise an ...
Aerodynamic Inverse Design and Shape Optimization via Control Theory
Aerodynamic Inverse Design Shape
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2015/6/18
Capability to predict the flow past an airplane in different flight regimes such as
take off, cruise, flutter.
2 Interactive design calculations to allow immediate improvement
3 A...
Aerodynamic Inverse Design and Shape Optimization via Control Theory
via Control Theory Shape
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2015/6/18
Capability to predict the flow past an airplane in different flight regimes such as
take off, cruise, flutter.
2 Interactive design calculations to allow immediate improvement
3 A...
A Sequel to Lighthill’s Early Work — Aerodynamic Inverse Design and Shape Optimization via Control Theory
Design and Shape via Control Theory
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2015/6/18
Capability to predict the flow past an airplane in different
flight regimes such as take off, cruise, flutter.
2 Interactive design calculations to allow immediate
imp...
高速滚珠轴承动态特性求解的沟道控制理论修正（Modification of Raceway Control Theory on the Dynamic Equations Group of High-speed Ball Bearing）
高速滚珠轴承 半经验摩擦因数 沟道控制理论
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2009/8/11
从滚珠轴承高速运转时滚动体（钢球）与内、外沟道接触存在旋滚比出发，分析了高速滚珠轴承动态方程组沟道控制理论的不足。在根据滚动体所受内外圈摩擦力与陀螺力矩相平衡的关系得出的内外沟道控制参数表达式中，引入滚动体与沟道之间摩擦因数的半经验公式。为避免沟道控制理论的不足，滚动体姿态角的计算采用了按照达朗伯原理推导的计算公式，取代了由沟道控制理论得出的姿态角。使得摩擦因数和姿态角的计算同时耦合了滚动体法向载...
天然气发动机怠速鲁棒控制（Idle Speed Control of CNG Engine Based on Robust Control Theory）
天然气发动机 怠速 H∞鲁棒控制 仿真 试验
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2009/5/22
将H∞鲁棒控制理论应用于天然气(CNG)发动机的怠速控制，建立了CNG发动机动力学模型，描述了发动机的不确定性。应用Matlab鲁棒控制工具箱，设计出基于H∞理论的CNG发动机怠速控制器，并进行了仿真分析和试验。仿真和台架试验表明，H∞控制具有很好的鲁棒性，提高了CNG发动机怠速工况的稳定性。
Investigation on Broaching-to Using Optimal Control Theory
Broaching Optimal Control Theory
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2009/4/10
Broaching-to is a phenomenon in which a ship cannot keep her desired course despite the maximum steering effort. Once this dangerous phenomenon happens, she could capsize due to violent yaw motion. Ge...