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检索条件"机构=Science and Technology on Altitude Simulation Laboratory"
43 条 记 录,以下是31-40 订阅
排序:
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
Finite-time Sliding Mode Control Method for a Class of Air Intake Testing Devices
Finite-time Sliding Mode Control Method for a Class of Air I...
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Artificial Intelligence and Intelligent Manufacturing (AIIM), International Symposium on
作者: Yunli Li Ming Pu Gexiang Zhang Zhihong Dan Song Zhang School of Automation Chengdu University of Information Technology Chengdu China Science and Technology on Altitude Simulation Laboratory AECC Sichuan Gas Turbine Establishment Mianyang China
This paper proposes a novel finite-time sliding mode control method for the enhancement of the velocity and precision in the control of temperature and pressure within a class of air intake testing devices. Initially,... 详细信息
来源: 评论
Adaptive Active Disturbance Rejection Control based on Coupling Coefficient with Applications to Flight Environment simulation System
Adaptive Active Disturbance Rejection Control based on Coupl...
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第43届中国控制会议
作者: Linfeng Wu Qiumeng Qian Chao Zhai Hehong Zhang School of Future Technology China University of Geosciences Science and Technology on Altitude Simulation Laboratory AECC Sichuan Gas Turbine Establishment College of Computer Science and Big Data Fuzhou University
The ability of a high-altitude test bench flight environment simulation system to accurately simulate high-altitude environmental parameters plays a crucial role in the performance testing and evaluation of aviation e... 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
A New Time Optimal Control based Tracking Differentiator with Small Phase Lag
A New Time Optimal Control based Tracking Differentiator wit...
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第43届中国控制会议
作者: Louyue Zhang Hehong Zhang Chao Zhai Xi Wang Zhihong Dan School of Energy and Power Engineering Beihang University College of Computer and Data Science Fuzhou University Science and Technology on Altitude Simulation Laboratory AECC Sichuan Gas Turbine Establishment Mianyang
Real-time filtering and derivative signals with as small phase lag as possible are of great significance for control performances. In this work, an enhanced time optimal control(referred as f sa) based tracking differ... 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
Design of Sliding Mode Extended State Observer for Active disturbance rejection control of Air Intake System
Design of Sliding Mode Extended State Observer for Active di...
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Artificial Intelligence and Intelligent Manufacturing (AIIM), International Symposium on
作者: Zezhen Zhou Haina Rong Tong Bi Gexiang Zhang Zhihong Dan Song Zhang School of Electrical Engineering Southwest Jiaotong University Chengdu China School of Automation Chengdu University of Information Technology Chengdu China Science and Technology on Altitude Simulation Laboratory AECC Sichuan Gas Turbine Establishment Mianyang China
The air intake control system is a key part of a type of propulsion system test bed. However, the existence of disturbances and random measurement noise in the control system, directly affect the reliability of the en... 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
Optimal Microphone Selection for Aero-Engine Acoustic Measurement
SSRN
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SSRN 2023年
作者: Li, Zepeng Qiao, Baijie Wen, Bi Chen, Xuefeng Jakobsson, Andreas School of Mechanical Engineering Xi’an Jiaotong University Xi’anCN-710049 China Department of Mathematical Statistics Lund University LundSE-22100 Sweden Science and Technology on Altitude Simulation Laboratory MianyangCN-621022 China
Acoustic testing is crucial in the aero-engine design process, providing valuable information about the sound field in terms of acoustic modes. The conventional use of a uniform sampling array limits the achievable re... 详细信息
来源: 评论
μ-Synthesis-based robust L1 adaptive control for aeropropulsion system test facility
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Aerospace science and technology 2023年 第1期140卷
作者: Liu, Jiashuai Wang, Xi Liu, Xi Zhu, Meiyin Pei, Xitong Dan, Zhihong Zhang, Song School of Energy and Power Engineering Beihang University Beijing100191 China Zhongfa Aviation Institute Beihang University Hangzhou311115 China Research Institute of Aero-Engine Beihang University Beijing100191 China Science and Technology on Altitude Simulation Laboratory AECC Sichuan Gas Turbine Establishment Mianyang621703 China
For Aeropropulsion System Test Facility (ASTF) applied in aero-engine performance testing, it is critical to accurately control the pressure and temperature of the airflow to simulate the flight environment. This arti... 详细信息
来源: 评论