Zobrazeno 1 - 10
of 18
pro vyhledávání: '"Zhihong Dan"'
Autor:
Keqiang Miao, Xi Wang, Meiyin Zhu, Song Zhang, Zhihong Dan, Jiashuai Liu, Shubo Yang, Xitong Pei, Xin Wang, Louyue Zhang
Publikováno v:
Symmetry, Vol 14, Iss 7, p 1399 (2022)
To solve the modeling problem of altitude ground test facility (AGTF) exhaust systems, which is caused by nonlinearity along the gas path and the difficulty of ejection factor calculation, a multi-cavity iterative modeling method is presented. The co
Externí odkaz:
https://doaj.org/article/69e46a5237fc478a94f85fb6e5639c00
Publikováno v:
Engineering Applications of Artificial Intelligence. 123:106475
Autor:
Huairong Chen, Keqiang Miao, Meiyin Zhu, Jiashuai Liu, Xi Wang, Nannan Gu, Song Zhang, Shubo Yang, Xitong Pei, Zhihong Dan
Publikováno v:
Chinese Journal of Aeronautics, Vol 34, Iss 2, Pp 420-431 (2021)
To solve the rapid transient control problem of Flight Environment Simulation System (FESS) of Altitude Ground Test Facilities (AGTF) with large heat transfer uncertainty and disturbance, a new adaptive control structure of modified robust optimal ad
Publikováno v:
Journal of Bionic Engineering. 17:708-717
The attitude control system of a flapping-wing flying robot plays an important role in the precise orientation and tracking of the robot. In this paper, the modeling of a bird-like micro flapping-wing system is introduced, and the design of a sliding
Publikováno v:
Processes; Volume 10; Issue 2; Pages: 377
The Flight Environment Simulation System (FESS) at Altitude Ground Test Facilities (AGTF) is used to test aircraft engines. The FESS model is the basis of research and verification of advanced control algorithms. To further improve the steady and dyn
Publikováno v:
Proceedings of 2021 International Conference on Autonomous Unmanned Systems (ICAUS 2021) ISBN: 9789811694912
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::631705dfc672bfd63e3b4e5efa25e7c3
https://doi.org/10.1007/978-981-16-9492-9_104
https://doi.org/10.1007/978-981-16-9492-9_104
To tackle the difficulty in tuning the parameters of sliding mode differentiator (SMD), an improved adaptive notch filter based real-time parameter tuning scheme (denoted as ANF-SMD) is presented. Specifically, the integral feedback of the system out
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::5cd26ca8058af3a52df5fc48e693fab2
https://hdl.handle.net/10356/169379
https://hdl.handle.net/10356/169379
Publikováno v:
Chinese Journal of Aeronautics, Vol 32, Iss 5, Pp 1204-1214 (2019)
To solve the problem of robust servo performance of Flight Environment Testbed (FET) of Altitude Ground Test Facilities (AGTF) over the whole operational envelope, a two-degree-of-freedom μ synthesis method based on Linear Parameter Varying (LPV) sc
Publikováno v:
Aerospace Science and Technology. 128:107787
Publikováno v:
2020 Chinese Automation Congress (CAC).
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 compare their performances in filterin