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浏览/检索结果: 共16条，第1-10条 帮助 条数/页： 5101520253035404550556065707580859095100 排序方式： 请选择题名升序题名降序提交时间升序提交时间降序作者升序作者降序发表日期升序发表日期降序 Nonsingular Terminal Sliding Mode Control With Ultra-Local Model and Single Input Interval Type-2 Fuzzy Logic Control for Pitch Control of Wind Turbines 期刊论文  OAI收割 IEEE/CAA Journal of Automatica Sinica, 2021, 卷号: 8, 期号: 3, 页码: 690-700 作者:  Saber Abrazeh;  Ahmad Parvaresh;  Saeid-Reza Mohseni;  Meisam Jahanshahi Zeitouni;  Meysam Gheisarnejad   |  收藏  |  浏览/下载：34/0  |  提交时间：2021/04/09 Interval type-2 (IT2) fuzzy logic control  model-independent nonsingular terminal sliding-mode control (MINTSMC)  pitch angle control  real-time software-in-the-loop (RT-SiL)   Structural analyses of the Group A flavin-dependent monooxygenase PieE reveal a sliding FAD cofactor conformation bridging OUT and IN conformations 期刊论文  OAI收割 JOURNAL OF BIOLOGICAL CHEMISTRY, 2020, 卷号: 295, 期号: 14, 页码: 4709, 4722 作者:  Manenda, Mahder S.;  Picard, Marie-Eve;  Zhang, Liping;  Cyr, Normand;  Zhu, Xiaojun   |  收藏  |  浏览/下载：72/0  |  提交时间：2020/09/22 flavin adenine dinucleotide (FAD)  enzyme catalysis  enzyme mechanism  small-angle X-ray scattering (SAXS)  crystal structure  flavin-dependent monooxygenase  hydroxylation  mobile flavin  piericidin  sliding conformation   Sliding Mode Guidance Law Considering Missile Dynamic Characteristics and Impact Angle Constraints 期刊论文  OAI收割 International Journal of Automation and Computing, 2018, 卷号: 15, 期号: 2, 页码: 218-227 作者:  Hui-Bo Zhou;  Jun-Hong Song;  Shen-Min Song   |  收藏  |  浏览/下载：17/0  |  提交时间：2021/02/23 Autopilot  impact angle  nonsingular terminal sliding mode  finite-time convergent  guidance.   Preparation of Dynamic Superhydrophobic Cotton Fabric via Radiation-induced Graft Polymerization 期刊论文  OAI收割 ACTA POLYMERICA SINICA, 2017, 期号: 2, 页码: 315-320 作者:  Li, JY;  Wang, ZQ;  Yu, M   |  收藏  |  浏览/下载：18/0  |  提交时间：2017/12/08 Dynamic Superhydrophobic  Radiation-induced Graft Polymerization  Cotton Fabrics  Sliding Angle   Durable superamphiphobic coatings repelling both cool and hot liquids based on carbon nanotubes 期刊论文  OAI收割 Journal of Colloid and Interface Science, 2017, 卷号: 505, 页码: 622-630 作者:  Fan L(范玲);  Zhai, Naihua;  Li LX(李凌霄);  Zhang JP(张俊平);  Zhang JP(张俊平)   |  收藏  |  浏览/下载：34/0  |  提交时间：2017/11/24 Superoleophobic  Silanes  Wettability  Carbon Nanotubes  Sliding Angle   多约束条件下末端制导律方法研究 学位论文  OAI收割 工学博士, 中国科学院自动化研究所: 中国科学院大学, 2015 作者:  李庆春 收藏  |  浏览/下载：178/0  |  提交时间：2015/09/02 末端制导  多约束条件  鲁棒制导律  模糊滑模变结构制导律  角度和时间协同制导  terminal guidance  multiple constraints  robust guidance law  fuzzy sliding mode control guidance law  impact angle and time cooperative guidance   几种超疏水表面的制备及其性能研究 学位论文  OAI收割 工学博士: 中国科学院研究生院, 2012 李健 收藏  |  浏览/下载：86/0  |  提交时间：2013/04/02 微纳米结构  超疏水  接触角  滚动角  黏附性  Micro/nanostructure  Superhydrophobicity  Contact angle  Sliding angle  Water adhesion   Microstructure-dependent mechanical behaviors of SiC nanowires 会议论文  OAI收割 23rd International Congress of Theoretical and Applied Mechanics, 中国北京/Beijing, China, 2012-08-19 作者:  Wang J;  Lu CS;  Wang Q;  Xiao P(肖攀);  Ke FJ(柯孚久) 收藏  |  浏览/下载：27/0  |  提交时间：2014/04/02 mechanical  dependent  their  oriented  observed  SIC  tensile  amorphous  brittleness  grains  sliding  angle  diverse  various  deformation  results  along   微纳米结构表面的构筑、表征及其超疏水性能研究 学位论文  OAI收割 工学博士: 中国科学院研究生院, 2011 郭永刚 收藏  |  浏览/下载：141/0  |  提交时间：2012/11/09 微纳米结构  超疏水  润湿性  接触角  滑动角  Micro/nano structure  Superhydrophobicity  Wettability  Contact angle  Sliding angle   Research on model reference sliding mode control in roll stabilization of aerocraft (EI CONFERENCE) 会议论文  OAI收割 2011 International Conference on Electric Information and Control Engineering, ICEICE 2011, April 15, 2011 - April 17, 2011, Wuhan, China Chu H.-R. 收藏  |  浏览/下载：40/0  |  提交时间：2013/03/25 Aimed at aerospace roll stabilization  control arithmetic based on model reference sliding mode variable structure theory and chattering reduction arithmetic are formulated. Correctness and validity of arithmetic are analyzed. With flight dynamics  the roll-loop mathematic model and reference model are established. Sliding hyperplane is deduced based on model reference sliding mode variable structure theory. Combing with reaching law  control law is derived  and stability of roll-loop is analyzed. Chattering of aileron instructions is alleviate by using boundary layer approach. Digital flying simulation result shows that variable structure control arithmetic realized roll stabilization control  the roll angle is less than 5.3 under powered flight  and that of unpowered flight is less than 0.5  respectively. The command fin angle is less than 1.5. High frequency chattering of fin command nearby the minimum velocity was trailed off by chattering reduction arithmetic. The sliding mode control arithmetic show good performance when aerodynamic coefficients varies 20%. The control arithmetic is easy to be implemented for its simplicity. 2011 IEEE.