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Fixed-Time Sliding Mode Control With Varying Exponent Coefficient for Modular Reconfigurable Flight Arrays 期刊论文
IEEE/CAA Journal of Automatica Sinica, 2024, 卷号: 11, 期号: 2, 页码: 514-528
作者:  Jianquan Yang;  Chunxi Yang;  Xiufeng Zhang;  Jing Na
收藏  |  浏览/下载：1/0  |  提交时间：2024/01/23
Longitudinal Control for Balloon-Borne Launched Solar Powered UAVs in Near-Space 期刊论文
JOURNAL OF SYSTEMS SCIENCE & COMPLEXITY, 2022, 卷号: 35, 期号: 3, 页码: 802-819
作者:  Hu Yanpeng;  Guo Jin;  Meng Wenyue;  Liu Guanyu;  Xue Wenchao
收藏  |  浏览/下载：9/0  |  提交时间：2023/02/07
UAV Dynamic Simulation Model Stablishment Method Based on Simulink/Aerosim 会议论文
2017 INTERNATIONAL CONFERENCE ON COMPUTER NETWORK, ELECTRONIC AND AUTOMATION (ICCNEA), 2017-01-01
作者:  Chen, Guoshao;  Wang, Zhongsheng;  Yang, Sen
收藏  |  浏览/下载：3/0  |  提交时间：2019/12/30
Flight dynamics study of a small tilt rotor UAV with tail propeller 会议论文
16th AIAA Aviation Technology, Integration, and Operations Conference
作者:  Wu, D.;  Li, H.;  Li, S.
收藏  |  浏览/下载：5/0  |  提交时间：2019/12/30
Aircraft flight simulation with landing gear based on multi-domain modeling technology (EI CONFERENCE) 会议论文
2012 2nd International Conference on Computer Application and System Modeling, ICCASM 2012, July 27, 2012 - July 29, 2012, Shenyang, China
Li M.; Hao X.; Han X.; Jia H.
收藏  |  浏览/下载：11/0  |  提交时间：2013/03/25
Three-loop autopilot design and simulation (EI CONFERENCE) 会议论文
2012 9th IEEE International Conference on Mechatronics and Automation, ICMA 2012, August 5, 2012 - August 8, 2012, Chengdu, China
Chu H.-R.; Zhang Y.
收藏  |  浏览/下载：39/0  |  提交时间：2013/03/25
In order to realize missile real-time change flight trajectory  three-loop autopilot is setting up. The structure characteristics  autopilot model  and control parameters design method were researched. Firstly  this paper introduced the 11th order three-loop autopilot model. With the principle of systems reduce model order  the 5th order model was deduced. On that basis  open-loop frequency characteristic and closed-loop frequency characteristic were analyzed. The variables of velocity ratio  dynamic pressure ratio and elevator efficiency ratio were leading to correct system nonlinear. And then autopilot gains design method were induced. System flight simulations were done  and result shows that autopilot gains played a good job in the flight trajectory  autopilot satisfied the flight index. 2012 IEEE.  
Lateral dynamic flight stability of hovering insects: theory vs. numerical simulation 期刊论文
ACTA MECHANICA SINICA, 2012, 卷号: 28, 页码: 221-231
作者:  Zhang, Yan-Lai;  Wu, Jiang-Hao;  Sun, Mao
收藏  |  浏览/下载：1/0  |  提交时间：2020/01/06
Establishment of airplane flight model and simulation analysis of landing behavior (EI CONFERENCE) 会议论文
2nd Annual Conference on Electrical and Control Engineering, ICECE 2011, September 16, 2011 - September 18, 2011, Yichang, China
Li M.; Li D.-W.; Jia H.-G.; Li L.
收藏  |  浏览/下载：17/0  |  提交时间：2013/03/25
This paper create a high fidelity plant model of an aircraft landing gear to inclusion into a full aircraft flight simulation for accurately analyzing the performance and influence of landing gear system. The use of domain specific modeling software enables detailed modeling of the physics and facilitates accurate computational simulation of the flight dynamic  aerodynamic  landing gear dynamic and mechanical loads that occur when the landing gear are deployed and retracted during landing and take-off operations. The parameter design space is easily searched by considering a number of different landing scenarios including touching down on one wheel first  to optimize the design. The simulation results show that the aircraft landing gear system mathematical model established appropriately reflects the change of force and moment in the process of taking off and landing  and it is actual in the physical process. 2011 IEEE.  
Aircraft landing gear simulation using multidomain modeling technology (EI CONFERENCE) 会议论文
2011 International Conference on Information Technology, Computer Engineering and Management Sciences, ICM 2011, September 24, 2011 - September 25, 2011, Nanjing, Jiangsu, China
Li M.; Hao X.-Y.; Han X.-F.; Jia H.-G.
收藏  |  浏览/下载：30/0  |  提交时间：2013/03/25
In order to accurately analyze the performance and influence of landing gear system  this paper presents a high fidelity plant model of an aircraft landing gear to inclusion into a full aircraft flight simulation. The use of domain specific modeling software enables detailed modeling of the physics and facilitates accurate computational simulation of the flight dynamic  aerodynamic  landing gear dynamic and mechanical loads that occur when the landing gear are deployed and retracted during landing and take-off operations. The parameter design space is easily searched by considering a number of different landing scenarios including touching down on one wheel first  to optimize the design. The simulation results show that the aircraft landing gear system mathematical model established appropriately reflects the change of force and moment in the process of taking off and landing  and it is improve the precision of flight simulation. 2011 IEEE.  
Modeling of a tilt rotor aircraft platform 期刊论文
2010, 2010
Yu Changjie; Zhu Jihong; Hu Chunhua; Sun Zengqi
收藏  |  浏览/下载：5/0

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