您的位置: 专家智库 > >

国家自然科学基金(91016004)

作品数:18 被引量:242H指数:7
相关作者:孙长银穆朝絮赵建辉李帆王伟更多>>
相关机构:北京航空航天大学东南大学天津大学更多>>
发文基金:国家自然科学基金国家杰出青年科学基金国家教育部博士点基金更多>>
相关领域:航空宇航科学技术自动化与计算机技术兵器科学与技术机械工程更多>>

文献类型

  • 18篇期刊文章
  • 9篇会议论文

领域

  • 14篇航空宇航科学...
  • 12篇自动化与计算...
  • 2篇兵器科学与技...
  • 1篇机械工程
  • 1篇理学

主题

  • 5篇飞行
  • 3篇飞行器
  • 3篇SLIDIN...
  • 3篇H
  • 2篇导弹
  • 2篇旋翼
  • 2篇子群
  • 2篇卫星
  • 2篇系统设计
  • 2篇粒子群
  • 2篇粒子群优化
  • 2篇滑模
  • 2篇滑模控制
  • 2篇混合粒子群
  • 2篇混合粒子群优...
  • 2篇观测器
  • 2篇航迹
  • 2篇航迹规划
  • 2篇航天
  • 2篇航天器

机构

  • 7篇北京航空航天...
  • 5篇东南大学
  • 3篇天津大学
  • 3篇南京信息工程...
  • 1篇北京科技大学
  • 1篇北京空间飞行...

作者

  • 4篇孙长银
  • 3篇李帆
  • 3篇赵建辉
  • 3篇穆朝絮
  • 2篇杨博
  • 2篇马浩
  • 2篇薛蕾
  • 2篇郝博
  • 2篇王伟
  • 1篇余瑶
  • 1篇王建青
  • 1篇郭雷
  • 1篇李小凤
  • 1篇杨照华
  • 1篇钱承山
  • 1篇余星火
  • 1篇万聪梅
  • 1篇徐金琦
  • 1篇冯云山
  • 1篇朱雪妍

传媒

  • 2篇宇航学报
  • 2篇自动化学报
  • 2篇Journa...
  • 2篇IEEE/C...
  • 1篇东南大学学报...
  • 1篇机械设计与制...
  • 1篇应用科学学报
  • 1篇弹箭与制导学...
  • 1篇飞行力学
  • 1篇科学技术与工...
  • 1篇Contro...
  • 1篇智能系统学报
  • 1篇空间控制技术...
  • 1篇Intern...

年份

  • 1篇2020
  • 1篇2018
  • 1篇2017
  • 1篇2016
  • 1篇2015
  • 1篇2014
  • 9篇2013
  • 9篇2012
  • 3篇2011
18 条 记 录,以下是 1-10
排序方式:
变时滞输入挠性航天器系统DOBC与H_∞复合控制方法
本文考虑含有时变输入时滞的挠性航天器姿态控制问题,采用干扰观测器与H∞相结合的复合控制方法,针对由挠性附件振动引起的干扰设计干扰观测器进行估计并前馈补偿,针对不同数量级的有界干扰分别选定不同的抑制率,设计H∞控制器以达到...
李小凤郭雷张玉民
关键词:挠性航天器干扰观测器
Second-order terminal sliding mode control for hypersonic vehicle in cruising flight with sliding mode disturbance observer被引量:22
2013年
This paper focuses on the design of nonlinear robust controller and disturbance observer for the longitudinal dynamics of a hypersonic vehicle (HSV) in the presence of parameter uncertainties and external disturbances. First, by combining terminal sliding mode control (TSMC) and second-order sliding mode control (SOSMC) approach, the second- order terminal sliding control (2TSMC) is proposed for the velocity and altitude tracking control of the HSV. The 2TSMC possesses the merits of both TSMC and SOSMC, which can provide fast convergence, continuous control law and high- tracking precision. Then, in order to increase the robustness of the control system and improve the control performance, the sliding mode disturbance observer (SMDO) is presented. The closed-loop stability is analyzed using the Lyapunov technique. Finally, simulation results illustrate the effectiveness of the proposed method, as well as the improved overall performance over the conventional sliding mode control (SMC).
Ruimin ZHANGChangyin SUNJingmei ZHANGYingjiang ZHOU
Recognition of vortex structures in turbulent refractive index field using wavelet transformation
2012年
When the light wave propagates through the hypersonic flow field, the aero-optic distortion happens. It is necessary to recognize the vortex structure for studying the light propagation model. A new vortex structure recognition method is proposed in this paper. Firstly, the refractive index field, which is transformed from the turbulent density field, is changed to gray scale images with a- bundant texture information equivalently. Then, wavelet transform is performed to decompose these images and the entropy values of the wavelet base coefficients are calculated. Comparing the entropy value to a given threshold, the modules with lower entropy are considered to be the large-scale vortex modules while those with higher entropy are small-scale vortex modules. The computer simulation results show that the proposed method is valid to recognize the vortex structures. This paper provides basis for investigation on the optics propagation model in terms of the turbulence vortex structures.
祁振强冯浩楠
多旋翼无人机标准化机体设计方法研究被引量:40
2014年
多旋翼无人机具有结构简单、可维护性强、无人员伤亡的优点,可广泛应用于航拍摄影、环境检测等领域,具有巨大的产业化前景。但多数科研机构大都注重飞行控制理论方面的研究,缺乏对机体设计的探讨,而这正是实现多旋翼无人机产业化的基础。从一个具体的设计实例出发,提出小型多旋翼无人机的标准化机体设计方法。然后通过对飞行控制系统的设计,实现多旋翼无人机的稳定飞行。飞行实验结果表明,设计的多旋翼无人机具有良好的稳定性能,从而验证机体设计和飞行控制方法的可行性。
王伟马浩徐金琦孙长银
关键词:无人机
模糊自适应的高超飞行器控制与干扰被引量:1
2012年
针对具有超大飞行马赫数、超宽飞行包络、飞行环境复杂等特点的高超声速飞行器,提出了基于模糊自适应的高超飞行器高度控制方法,分别设计了高度和速度控制器.针对所设计的控制器,分析了气动干扰力矩、测量噪声、舵机干扰、气动参数不确定性和飞行器模型参数不确定性对飞行器高度控制和速度控制效果的影响,然后又分析了综合考虑以上干扰和不确定性对飞行器高度控制和速度控制效果的影响.仿真结果表明,对各种干扰和不确定性,所设计的控制器速度和高度控制有较好的跟踪性和鲁棒性,达到了满意的效果.
冯云山杨照华
关键词:模糊自适应高超声速飞行器不确定性
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
文献传递
近空间高超声速飞行器控制的几个科学问题研究被引量:85
2013年
近空间高超声速飞行器的特点给其建模和控制带来了新的问题.本文首先分析高超声速飞行器的特点,进一步给出大包络飞行的统一模型.其次,总结了高超声速飞行器巡航控制、再入姿态控制研究的现状,强调了弹性、非最小相位、再入制导控制一体化设计等问题.最后,结合高超声速飞行器的发展,阐述了高超声速目标的拦截问题,提供未来可供研究的方向.
孙长银穆朝絮余瑶
关键词:高超声速飞行器特性分析巡航控制拦截
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
Consensus Tracking for Multi-Vehicle System with a Well-Informed Leader:Adaptive Control Method
By referring to adaptive control method,the consensus tracking problem for multi-vehicle system with a well-in...
JingMei ZHANG,Li WANG,Jianwei XIA are with School of Automation,Southeast University,Nanjing,210096 China.ChangYin SUN is with the school of Automation,Southeast University.He is currently a full time Professor.His major research fields are nonlinear control,intelligence control and pattern recognition.
文献传递
大气湍流对平流层星光导航中星光传输的影响被引量:2
2017年
以平流层飞行器用星光导航为背景,研究在平流层内星光传输过程受大气湍流的影响机理,揭示平流层中星光的衰减规律,为建立平流层星光导航星库以及电耦合器件(CCD)所摄取的星图补偿方法提供理论依据。研究提出将流场密度和流场密度脉动变化大的区域划分为宽度为L的特性截面,并基于几何光学法及统计光学理论分别计算星光穿过各特性截面后产生的光线偏折及平均光强衰减,进而推导整个平流层内星光传输过程中的能量衰减变化曲线。采用基于k-ε双方程湍流模型的雷诺平均法计算不同极端情况下的大气湍流场密度及密度脉动分布。通过计算机数值仿真表明:星光穿过具有湍流的平流层时将发生明显偏折,其偏折程度与流场密度值有关;同时星光光强衰减,衰减程度与流场密度脉动值有关。
杨博朱雪妍
关键词:大气湍流星等
共3页<123>
聚类工具0