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检索条件"机构=Science and Technology on Altitude Simulation Laboratory"
42 条 记 录,以下是31-40 订阅
排序:
A Light-Weight Prediction Model for Aero-Engine Surge Based on Seq2Seq  7th
A Light-Weight Prediction Model for Aero-Engine Surge Based ...
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7th International Conference on Artificial Intelligence and Security, ICAIS 2021
作者: Peng, Yu Li, Xiaoyu Lu, Chao Tang, Xiaolan Lin, Bin School of Information and Software Engineering University of Electronic Science and Technology of China Chengdu610054 China Science and Technology on Altitude Simulation Laboratory Sichuan Gas Turbine Establishment Aero Engine Corporation of China Mianyang621000 China School of Computer Science Southwest Petroleum University Chengdu610500 China School of Engineering Sichuan Normal University Chengdu610066 China
Surge is an abnormal fault caused by compressor in the process of aero-engine flight, which will reduce the performance of aero-engines. When the surge gets serious, it will even cause engine damage, endanger flight s... 详细信息
来源: 评论
Active disturbance rejection intake pressure control of aeropropulsion systems test facility with adaptive parameter b0
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Aerospace science and technology 2025年 163卷
作者: Xu, Zhuang Zhang, Hehong Zhai, Chao Xiao, Gaoxi Qian, Qiumeng Huang, Feng College of Computer and Data Science Fuzhou University Fuzhou350108 China Wuhan430074 China School of Electrical and Electronic Engineering Nanyang Technological University Singapore639798 Singapore Science and Technology on Altitude Simulation Laboratory AECC Sichuan Gas Turbine Establishment Mianyang621703 China School of Mechanical Engineering and Automation Fuzhou University Fuzhou350108 China
Establishing a precise intake pressure environment in the aeropropulsion systems test facility (ASTF) is critical for evaluating aeroengines' flight characteristics. The model-partial and robust active disturbance... 详细信息
来源: 评论
A Model Average Algorithm for Housing Price Forecast with Evaluation Interpretation
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Journal of Quantum Computing 2022年 第3期4卷 147-163页
作者: Jintao Fu Yong Zhou Qian Qiu Guangwei Xu Neng Wan School of Computer Science Southwest Petroleum UniversityChengdu610500China Key Laboratory on Aero-Engine Altitude Simulation Technology Sichuan Gas Turbine EstablishmentAECCMianyang621000China Aero Engine Academy of China Aero Engine Corporation of ChinaBeijing101300China
In the field of computer research,the increase of data in result of societal progress has been remarkable,and the management of this data and the analysis of linked businesses have grown in *** are numerous practical ... 详细信息
来源: 评论
An Adaptive Formulation-based Many-Objective Evolutionary Algorithm for Multi-Scenario Optimization in Data Enrichment
An Adaptive Formulation-based Many-Objective Evolutionary Al...
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Congress on Evolutionary Computation
作者: Liang Fan Xudong Feng Handing Wang School of Artificial Intelligence Xidian University Xi'an China Science and Technology on Altitude Simulation Laboratory AECC Sichuan Gas Turbine Establishment Mianyang China
In many practical applications, data enrichment can generate a large amount of accurate data to alleviate the problem of data scarcity. In order to make the fake data generated in data enrichment as close to the real ... 详细信息
来源: 评论
Extended State Observer based Attitude Control of a Bird-like Flapping-wing Flying Robot
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Journal of Bionic Engineering 2020年 第4期17卷 708-717页
作者: Keqiang Bai YunZhi Luo Zhihong Dan Song Zhang Meiling Wang Qiumeng Qian Jun Zhong School of Information Engineering Southwest University of Science and TechnologyRobot Technology Used for Special Environment Key Laboratory of Sichuan ProvinceMianyang 621010China Automation Research Institute Co. Ltd.of China South Industries Group CorporationMianyang 621000China Science and Technology on Altitude Simulation Laboratory AECC Sichuan Gas Turbine EstablishmentMianyang 621703China AECC Sichuan Gas Turbine Establishment Mianyang 621703China Chinese Academy of Sciences Hefei Institutes of Physical Science Hefei 230022China College of Mechanical and Electrical Engineering Hohai UniversityChangzhou 213022China
The attitude control system of a flapping-wing flying robot plays an important role in the precise orientation and tracking of the *** this paper,the modeling of a bird-like micro flapping-wing system is introduced,an... 详细信息
来源: 评论
Multi-dimensional simulations for extensive off-design conditions of gas turbines by iterative-coupled methods using different characteristic maps of coaxial compressor and turbine
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Case Studies in Thermal Engineering 2025年 72卷
作者: Weimin Deng Guangming Ren Linyuan Jia Zuojun Wei Yuchun Chen Xiaohua Gan School of Power and Energy Northwestern Polytechnical University Xi'an 710072 China Department of Mechanics and Aerospace Engineering Southern University of Science and Technology Shenzhen 518055 China Science and Technology on Altitude Simulation Laboratory Mianyang 621000 China Shenzhen Key Laboratory of Wide-Speed-Range and Variable-Density Continuous Wind Tunnel Southern University of Science and Technology Shenzhen 518000 China National Key Laboratory of Science and Technology on Advanced Light-duty Gas-turbine Xi'an 710129 China
Multi-dimensional simulations offer a complementary numerical platform to gas turbine experimentation, generating supportive data for training adaptation and artificial intelligence models. However, the application of... 详细信息
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Aerodynamic modeling and transient performance improvement of a free jet altitude test facility  6th
Aerodynamic modeling and transient performance improvement o...
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6th International Conference on Artificial Intelligence and Security,ICAIS 2020
作者: Wu, Feng Gao, Limin Wu, Xinyun Feng, Xudong Leng, Lintao Li, Yaoyu School of Power and Energy Northwestern Polytechnical University Xi’an710072 China The National Key Laboratory of Aerodynamic Design and Research Xi’an710129 China School of Information and Software Engineering University of Electronic Science and Technology of China Chengdu610054 China Key Laboratory of Science and Technology on Aero-Eigine Altitude Simulation AECC Sichuan Gas Turbine Establishment Chengdu610000 China
An inlet-engine altitude test facility for flight condition simulation is modeled for the system dynamic performance improvement. The system model equations are solved with an improved Euler integral method. To simula... 详细信息
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Nonlinear PID Pressure Control Based on Extremum Seeking
Nonlinear PID Pressure Control Based on Extremum Seeking
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第三十九届中国控制会议
作者: Song Zhang Zhihong Dan Qiumeng Qian Yuying Guo Jianping Zhang AECC Sichuan Gas Turbine Establishment Science and Technology on Altitude Simulation Laboratory School of Information Engineering Southwest University of Science and Technology School of Manufacturing Science and Engineering Southwest University of Science and Technology
Rear-cabin pressure control system of high-altitude test facility has the characteristics of large time-delay, nonlinearity and strong disturbances. In China, the rear-cabin pressure control system uses the convention... 详细信息
来源: 评论
A Comparison Study of Tracking Differentiator and Robust Exact Differentiator
A Comparison Study of Tracking Differentiator and Robust Exa...
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Chinese Automation Congress (CAC)
作者: Juan Wang Hehong Zhang Gaoxi Xiao Zhihong Dan Song Zhang Yunde Xie College of Mathematics and Computer Science Fuzhou University Fuzhou China School of Electrical and Electronic Engineering Nanyang Technological University Singapore Singapore Singapore Science and Technology on Altitude Simulation Laboratory AECC Sichuan Gas Turbine Establishment of China Mianyang China Beijing Rail Transit Technology Equipment Group Co. Ltd Beijing China
This paper presents a comparison study of two commonly-used differentiators, namely tracking differentiator (TD) and robust exact differentiator (RED) in both the frequency and the time domains. Specifically, we compa... 详细信息
来源: 评论
EFFECT OF THE RIM SEAL CONFIGURATIONS ON THE HOT GAS INGESTION INTO THE ROTOR-STATOR CAVITY
EFFECT OF THE RIM SEAL CONFIGURATIONS ON THE HOT GAS INGESTI...
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第三届中国国际透平机械学术会议
作者: Xing-yun Jia Jie Zhou Qun Zheng Hai Zhang College of Power and Energy Engineering Harbin Engineering UniversityHarbin 150001China Science and Technology on Altitude Simulation Laboratory China Gas Turbine EstablishmentChina Aviat
The effect of rim seal configurations on the flow and heat transfer characteristics in a turbine cavity and the rim seal clearance flow are computed by using a numerical method for conjugate heat transfer.A radial cle... 详细信息
来源: 评论