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国家教育部博士点基金(20110092110020)

作品数:5 被引量:84H指数:4
相关作者:穆朝絮余星火张兰孙长银余瑶更多>>
相关机构:东南大学天津大学北京科技大学更多>>
发文基金:国家教育部博士点基金国家自然科学基金国家杰出青年科学基金更多>>
相关领域:航空宇航科学技术自动化与计算机技术更多>>

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Non-fragile switching tracking control for a flexible air-breathing hypersonic vehicle based on polytopic LPV model被引量:21
2013年
This article proposes a linear parameter varying (LPV) switching tracking control scheme for a flexible air-breathing hypersonic vehicle (FAHV). First, a polytopic LPV model is constructed to represent the complex nonlinear longitudinal model of the FAHV by using Jacobian linearization and tensor-product (T-P) model transformation approach. Second, for less conservative controller design purpose, the flight envelope is divided into four sub-regions and a non-fragile LPV controller is designed for each parameter sub-region. These non-fragile LPV controllers are then switched in order to guarantee the closed-loop FAHV system to be asymptotically stable and satisfy a specified performance criterion. The desired non-fragile LPV switching controller is found by solving a convex constraint problem which can be efficiently solved using available linear matrix inequality (LMI) techniques, and robust stability analysis of the closed-loop FAHV system is verified based on multiple Lypapunov functions (MLFs). Finally, numerical simulations have demonstrated the effectiveness of the proposed approach.
Huang YiqingSun ChangyinQian ChengshanWang Li
异构无人机群鲁棒一致性协议设计被引量:1
2015年
研究了具有非线性不确定性的异构无人机群系统分布式一致性跟踪控制问题.文中假设领航者的输出是时变的,无人机自主体具有不同的非线性不确定空气动力特性,设计分布式鲁棒一致性协议,抑制非线性不确定性对闭环系统的影响,使得跟随者可以跟随领航者.所设计的鲁棒一致性协议包括标称控制器和鲁棒补偿器两部分,标称控制器的设计是为了使标称的无人机群具有一致性跟踪特性,鲁棒补偿器的设计是为了抑制不确定性对系统的影响,文中用李雅普诺夫函数分析并证明了一致性误差能以期望的速度收敛到原点任意小的邻域.最后,通过仿真验证了一致性协议的有效性.
孙长银余瑶张兰
Polytopic LPV Gain-scheduled Control for a Flexible Air-breathing Hypersonic Vehicle
<正>This article investigates polytopic Linear Parameter Varying(LPV) modeling and control problem for a flexib...
HUANG Yiqing~1
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Adaptive Sliding Mode Control for Re-entry Attitude of Near Space Hypersonic Vehicle Based on Backstepping Design被引量:30
2015年
Combining sliding mode control method with radial basis function neural network (RBFNN), this paper proposes a robust adaptive control scheme based on backstepping design for re-entry attitude tracking control of near space hypersonic vehicle (NSHV) in the presence of parameter variations and external disturbances. In the attitude angle loop, a robust adaptive virtual control law is designed by using the adaptive method to estimate the unknown upper bound of the compound uncertainties. In the angular velocity loop, an adaptive sliding mode control law is designed to suppress the effect of parameter variations and external disturbances. The main benefit of the sliding mode control is robustness to parameter variations and external disturbances. To further improve the control performance, RBFNNs are introduced to approximate the compound uncertainties in the attitude angle loop and angular velocity loop, respectively. Based on Lyapunov stability theory, the tracking errors are shown to be asymptotically stable. Simulation results show that the proposed control system attains a satisfied control performance and is robust against parameter variations and external disturbances. © 2014 Chinese Association of Automation.
Jingmei ZhangChangyin SunRuimin ZhangChengshan Qian
关键词:AIRSHIPSBACKSTEPPING
Fast Smooth Second Order Sliding Mode Control Design for Near-Space Hypersonic Vehicle’s Re-entry Attitude
This paper deals with the attitude control problem for a near-space hypersonic vehicle(NHV) subject to strong ...
ZHANG Ruimin~(1
非奇异终端滑模控制系统相轨迹和暂态分析被引量:27
2013年
对于采用非奇异终端滑模控制的二阶系统,考虑到不同的初始状态,研究了其相轨迹的分布规律,给出了临界曲面的概念和解析表达.基于相轨迹的分布,考虑了系统初始状态与到达滑模面时间的关系,探讨了到达时间最大值的估计算法,并给出了非奇异终端滑模控制系统的收敛时间的数学表达.通过仿真验证了相轨迹的分布规律和临界曲面的正确性,以及根据系统初值估计到达时间的有效性.
穆朝絮余星火孙长银
关键词:非奇异终端滑模收敛性
Robust Attitude Decentralized Tracking Control for a 3-DOF Helicopter with Unknown Input Time-delay
Robust attitude decentralized tracking control problem for a 3-DOF helicopter is investigated. The model of th...
Yao YuChang-Yin Sun
关键词:BACKSTEPPINGROBUST
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Polytopic LPV modeling and gain-scheduled switching control for a flexible air-breathing hypersonic vehicle被引量:10
2013年
A novel gain-scheduled switching control method for the longitudinal motion of a flexible air-breathing hypersonic vehicle (FAHV) is proposed. Firstly, velocity and altitude are selected as scheduling variables, a polytopic linear parameter varying (LPV) model is developed to represent the complex nonlinear longitudinal dynamics of the FAHV. Secondly, based on the obtained polytopic LPV model, the flight envelope is divided into four smaller subregions, and four gain-scheduled controllers are designed for these parameter subregions. Then, by the defined switching characteristic function, these gain-scheduled controllers are switched in order to guarantee the closed-loop FAHV system to be asymptotically stable and satisfy a given tracking error performance criterion. The condition of gain-scheduled switching controller synthesis is given in terms of linear matrix inequalities (LMIs) which can be easily solved by using standard software packages. Finally, simulation results show the effectiveness of the presented method.
Yiqing HuangChangyin SunChengshan QianJingmei ZhangLi Wang
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