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检索条件"机构=Science and Technology On Space Intelligent Control Laboratory"
6066 条 记 录,以下是4891-4900 订阅
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A novel saturated attitude controller for rigid body subject to bounded external disturbances  34
A novel saturated attitude controller for rigid body subject...
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第三十四届中国控制会议
作者: HU Jinchang Zhang Honghua Beijing Institute of Control Engineering Science and Technology on Space Intelligent Control Laboratory
We propose a new smooth attitude controller for rigid body in the presence of input saturation and external *** controller is composed of three parts,i.e.,the quaternion part,the saturated velocity part,and the bounde... 详细信息
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Approach and Landing Guidance Based on Sliding Mode control and Input-to-State Stability  34
Approach and Landing Guidance Based on Sliding Mode Control ...
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第三十四届中国控制会议
作者: YAN Han TAN Shuping Science and Technology on Space Intelligent Control Laboratory Beijing Institute of Control Engineering
This paper presents a new guidance law based on sliding-mode control and input-to-state stability(ISS) for approach and landing of a reusable launch vehicle(RLV). According to the idea of reference-trajectory guidance... 详细信息
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Autonomous optical navigation approach aided by radio beacon for deep space spacecraft  28
Autonomous optical navigation approach aided by radio beacon...
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28th Chinese control and Decision Conference, CCDC 2016
作者: Yan, Jing Shengying, Zhu Lina, Wang School of Aerospace Engineering Beijing Institute of Technology Beijing100081 China Key Laboratory of Autonomous Navigation and Control for Deep Space Exploration Ministry of Industry and Information Technology Beijing100081 China Key Laboratory of Dynamics and Control of Flight Vehicle Ministry of Education Beijing100081 China National Key Laboratory of Science and Technology on Aerospace Intelligence Control Beijing100854 China
According to task requests of deep space exploration approach phase such as autonomy, real-time and so on, we did a research into the problem of autonomous navigation at this approach phase and put forward an autonomo... 详细信息
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Actuators Coupled Design Based Adaptive Backstepping control of Air-breathing Hypersonic Vehicle
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IFAC-PapersOnLine 2015年 第28期48卷 508-513页
作者: Li, Gongjun Meng, Bin Beijing Institute of Control Engineering Beijing100190 China Science and Technology on Space Intelligent Control Laboratory Beijing100190 China
In this paper, we study the robust design of the flight control system for the longitudinal dynamics of air-breathing hypersonic vehicles. First, the longitudinal dynamics model is divided into the velocity subsystem ... 详细信息
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Design of online water quality monitoring system and prediction based on probabilistic neural network
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International Journal of Wireless and Mobile Computing 2016年 第4期10卷 371-377页
作者: Dai, Lu Chen, Xiong Intelligent Control Research Laboratory School of Information Science and Technology Fudan University Shanghai China
Online water quality monitoring systems have many significant benefits in fields such as source water protection, water treatment, and wastewater discharge, and in accidental or deliberate event of water contamination... 详细信息
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Generalised Error Functions from the Kerr Metric
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Chinese Physics Letters 2016年 第3期33卷 12-16页
作者: 唐文林 罗子人 刘润球 Science and Technology on Aerospace Flight Dynamics Laboratory Beijing Aerospace Control Center Department of Aerospace Guidance Navigation and Control School of AstronauticsBeihang University QUEST Center of Quantum Engineering and Space-Time Research Leibniz Universitt Hannover Max Planck Institute for Gravitational Physics(Albert Einstein Institute) Institute of Applied Mathematics Morningside Center of Mathematics and LESCInstitute of Computational MathematicsAcademy of Mathematics and System ScienceChinese Academy of Sciences
Motivated by the effort to understand the mathematical structure underlying the Teukolsky equations in a Kerr metric background, a homogeneous integral equation related to the prolate spheroidal function is studied. F... 详细信息
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Fuel-Optimal Trajectory Optimization for Lunar Soft Landing via Enhanced Simultaneous Dynamic Optimization Approach
Fuel-Optimal Trajectory Optimization for Lunar Soft Landing ...
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2016 IEEE Chinese Guidance, Navigation and control Conference (IEEE CGNCC2016)
作者: Lin Ma Zhengyu Song Zhijiang Shao College of Control Science and Engineering Zhejiang University National Key Laboratory of Science and Technology on Aerospace Intelligent Control
In this study,the fuel-optimal trajectory optimization problem of lunar soft landing using variable-thrust propulsion is ***,we formulate the trajectory optimization problem of lunar soft landing with three-dimensiona... 详细信息
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The Development of A Novel Servo Motor controller Based on EtherCAT and FPGA
The Development of A Novel Servo Motor Controller Based on E...
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第28届中国控制与决策会议
作者: Jianjun Liu Songlin Chen Guojiang Zhang Lei Shi Control and Simulation Center Harbin Institute of Technology Beijing Control Engineering Research Institute Key Laboratory of space intelligent control
This paper focuses on the design of a novel SMC(servo motor controller) based on EtherCAT in order to realize flexible networked multi-axis motion control with low cost and high *** is chosen as only kernel component ... 详细信息
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An evolutionary potential game theoretic approach for the K-COVER problem in multi-UAV sensor networks
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Zhongguo Kexue Jishu Kexue/Scientia Sinica Technologica 2016年 第10期46卷 1016-1023页
作者: Sun, Changhao Duan, Haibin Bio-inspired Autonomous Flight Systems Research Group Science and Technology on Aircraft Control Laboratory Beihang University Beijing100191 China Qian Xuesen Laboratory of Space Technology China Academy of Space Technology Beijing100094 China
This paper focuses on the K-COVER problem in unmanned aerial vehicle (UAV) sensor networks and proposes a game theoretic approach based on the network potential game and Log-linear learning. After detailing the resear... 详细信息
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Design of Distributed and Autonomous Test System Based on B/S Mode
Design of Distributed and Autonomous Test System Based on B/...
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2016 3rd International Conference on Engineering technology and Application(ICETA 2016)
作者: Juan Chen Yuan Li Wanguo Li Youwei Zhu Xiaojian Zhang Junwei Zhao Science and Technology on Aerospace Intelligent Control Laboratory Beijing University of Aeronautics and Astronautics
With the transformation of military tactic to informatization and networking and the need of rapid processing and measurement of mass of data,the measurement system of missile launch system is important to guarantee t... 详细信息
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