Zobrazeno 1 - 10
of 2 428
pro vyhledávání: '"flight envelope"'
Publikováno v:
Научный вестник МГТУ ГА, Vol 27, Iss 3, Pp 35-49 (2024)
With the publication of this article, the authors continue the research on the development and testing of a methodology for in-flight aircraft rerouting which have begun in previously published articles in the Civil Aviation High Technologies of the
Externí odkaz:
https://doaj.org/article/3f7c6327fda04230992ed487254bd0c1
Autor:
P. S. Kostin, K. A. Zhuravskiy
Publikováno v:
Научный вестник МГТУ ГА, Vol 26, Iss 4, Pp 77-92 (2023)
The article substantiates the relevance to develop an analytical-simulation model of fighter flight dynamics with a limiter for the permissible flight envelope during the split-S maneuver. The structure of the analytical and simulation model of a fig
Externí odkaz:
https://doaj.org/article/4b4f07bfa6c84d6f95493e7b2dc78ecc
Autor:
JIANG Yunshen, CAI Kailong
Publikováno v:
Hangkong gongcheng jinzhan, Vol 14, Iss 3, Pp 77-83 (2023)
In the process of robust controller design for aircraft engines, it is difficult to divide the flight envelope re-gion systematically. In this paper, the flight envelope division methods for aircraft engines based on thrust fuel con-sumption rate cha
Externí odkaz:
https://doaj.org/article/089b447c382348e1bcee802dc28cde3a
Autor:
K. A. Zhuravsky, P. S. Kostin
Publikováno v:
Научный вестник МГТУ ГА, Vol 25, Iss 6, Pp 77-90 (2023)
Due to a steady extension of the flight envelope of modern agile combat aircraft, with the growing requirements for state tests, it is increasingly necessary to study the entire flight envelope and specifically, to determine the main performance data
Externí odkaz:
https://doaj.org/article/954eea468f08409994d3ca03b82a6d97
Publikováno v:
Aerospace, Vol 11, Iss 2, p 160 (2024)
In hostile environments, engine damage is of particular concern since the engine is the only component to generate thrust that affects survivability. For an aircraft suffering thrust failure, the forced landing sites should be identified within the g
Externí odkaz:
https://doaj.org/article/660b4c3de4fc44b39ce2cd73293f3818
Akademický článek
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Autor:
WANG Chunyang, ZHOU Zhou
Publikováno v:
Hangkong gongcheng jinzhan, Vol 13, Iss 1, Pp 42-50 (2022)
The accurate description of the transition corridor is important for vertical take-off and landing(VTOL)fixed-wing unmanned aerial vehicle(UAV)flight. In order to study the transitional flight process of VTOL fixedwing UAV,a transition corridor model
Externí odkaz:
https://doaj.org/article/a493a90842044762a57852ee8ed6078b
Autor:
Yasin ŞÖHRET, Ali DİNÇ
Publikováno v:
Havacılık ve Uzay Teknolojileri Dergisi, Vol 15, Iss 1, Pp 35-45 (2022)
In this study, exergy mapping of an unmanned aerial vehicle (UAV) is investigated during its reconnaissance flight. A turboprop UAV is selected for the application of the exergy of lift method covering a full flight envelope (from takeoff to landing)
Externí odkaz:
https://doaj.org/article/683e6b60961b437c904200199faaba4b
Akademický článek
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Autor:
Muhammad Uzair Hassan, Ahsan Ali
Publikováno v:
Pakistan Journal of Engineering & Technology, Vol 5, Iss 2 (2022)
A new approach to cater abrupt gain switching at boundaries of steady-state trim points in Conventional Gain Scheduling (CGS) applied to aircraft flight control applications. The primary purpose of this research is to improve the stability properties
Externí odkaz:
https://doaj.org/article/d54178ccf4fb4e7896266f3234460f3f