Zobrazeno 1 - 10
of 10
pro vyhledávání: '"Mudassir Lone"'
Publikováno v:
Aviation, Vol 20, Iss 4 (2016)
The flight dynamics and handling qualities of any flexible aircraft can be analysed within the Cranfield Aircraft Accelerated Loads Model (CA2LM) framework. The modelling techniques and methods used to develop the framework are presented. The aerodyn
Externí odkaz:
https://doaj.org/article/4930729cb3754772944dd47de17bbaad
Publikováno v:
Aerospace, Vol 6, Iss 6, p 70 (2019)
A slalom and alignment tracking manoeuvre was developed for multi-directional handling qualities analysis of large transport aircraft in simulation environments. The manoeuvre is defined and scaled as a function of aircraft characteristics, flight co
Externí odkaz:
https://doaj.org/article/4be97c4b79f244bb879a98a99d5f6b34
Publikováno v:
Aerospace, Vol 6, Iss 6, p 63 (2019)
Wingtip folding is a means by which an aircraft’s wingspan can be extended, allowing designers to take advantage of the associated reduction in induced drag. This type of device can provide other benefits if used in flight, such as flight control a
Externí odkaz:
https://doaj.org/article/bd482adb25634c97b33518fd93a3117d
Autor:
Shivali Slathia, Rakesh Kumar, Mudassir Lone, Wattana Viriyasitavat, Amandeep Kaur, Gaurav Dhiman
Publikováno v:
Lecture Notes in Networks and Systems ISBN: 9789811992278
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8bc120f0026b5582909ae969675ec72e
https://doi.org/10.1007/978-981-19-9228-5_56
https://doi.org/10.1007/978-981-19-9228-5_56
Publikováno v:
Engineering Psychology and Cognitive Ergonomics ISBN: 9783031060854
There are different designs of inceptors applied in the modern flight deck. How do pilots define how to precisely control the aircraft as their intention? Ten pilots have been asked to take part in the flight simulation trials. They were given tasks
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d3aaad8e2ba180ab998ca0aca0636ff7
https://dspace.lib.cranfield.ac.uk/handle/1826/18352
https://dspace.lib.cranfield.ac.uk/handle/1826/18352
Autor:
Thomas Kissinger, Stephen W James, Simone Weber, Kevin Mullaney, Edmond Chehura, Huseyin H Pekmezci, James H Barrington, Stephen E Staines, Thomas O H Charrett, Nicholas J Lawson, Mudassir Lone, Richard Atack, Ralph P Tatam
Optical fibre strain and shape measurement sensors were deployed on a rotor blade during a full-speed helicopter ground run, with real-time data wirelessly streamed from rotor hub-mounted sensor interrogators. In part 2 of a 2-part paper series, two-
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8a8055b15e3c05ae8642b9f9fbef140a
http://dspace.lib.cranfield.ac.uk/handle/1826/18004
http://dspace.lib.cranfield.ac.uk/handle/1826/18004
Autor:
Stephen W James, Thomas Kissinger, Simone Weber, Kevin Mullaney, Edmond Chehura, Huseyin H Pekmezci, James H Barrington, Stephen E Staines, Thomas O H Charrett, Nicholas J Lawson, Mudassir Lone, Richard Atack, Ralph P Tatam
Optical fibre strain and shape measurement sensors were deployed on a 5-m long rotor blade during a full-speed (rotation rate 6.6 Hz) helicopter ground run, with real-time data wirelessly streamed from rotor hub-mounted sensor interrogators. In Part
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a7b4d3cc8fcacea9e5ca159242ae6613
https://dspace.lib.cranfield.ac.uk/handle/1826/18003
https://dspace.lib.cranfield.ac.uk/handle/1826/18003
Publikováno v:
Journal of Aerospace Engineering. 35
Publikováno v:
Aerospace Medicine and Human Performance. 91:767-775
BACKGROUND: The risks posed by flight illusions impacting pilot spatial orientation have been determined as a safety concern from numerous past aviation accident investigations. Early demonstration of the adverse effects of flight illusions on spatia
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 231:1183-1198
Artificial neural networks are an established technique for constructing non-linear models of multi-input–multi-output systems based on sets of observations. In terms of aerospace vehicle modeling, however, these are currently restricted to either