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Publikováno v:
In Chinese Journal of Aeronautics April 2011 24(2):150-163
Publikováno v:
Journal of Aerospace Technology and Management, Vol 5, Iss 3 (2013)
http://dx.doi.org/10.5028/jatm.v5i3.225 In this paper, a multidisciplinary design optimization (MDO) approach of a solid propellant kick rocket motor is considered. A genetic algorithm optimization method has been used. The optimized kick solid rock
Externí odkaz:
https://doaj.org/article/284f4d2331514987882ffada90984837
Publikováno v:
The Aeronautical Journal. 121:469-487
In this work, trajectory optimisation has been performed for a wing-body rocket assisted vehicle to compute the bestset of performance parameters including burn-out angle, angle-of-attack, bank-angle and throttle command that would result in optimal
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8c6eaaa8b86d319eb3ac5bf586c6b2f8
https://doi.org/10.1017/aer.2017.11
https://doi.org/10.1017/aer.2017.11
Publikováno v:
Aircraft Engineering and Aerospace Technology. 87:67-78
Purpose – The purpose of the paper is to study the variation of optimal burnout angle at the end of the ascent phase and the optimal control deflection during the glide phase, that would maximize the downrange performance of a hypersonic boost-glid
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9d5a159c76ba9ac007aa86d43781644e
https://doi.org/10.1108/aeat-04-2013-0079
https://doi.org/10.1108/aeat-04-2013-0079
Publikováno v:
Journal of Aerospace Technology & Management. Jul-Sep2014, Vol. 6 Issue 3, p291-300. 10p.
Publikováno v:
Journal of Aerospace Technology & Management. Jul-Sep2013, Vol. 5 Issue 3, p293-304. 12p.
Publikováno v:
Acta Astronautica. 67:826-844
Satellite launch vehicle design lies at the cross-road of multiple challenging technologies and its design and optimization presents a typical example of multidisciplinary design and optimization process. The complexity of problem demands for highly
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::df7640f265b2f08a21cd9ca34c36c431
https://doi.org/10.1016/j.actaastro.2010.05.016
https://doi.org/10.1016/j.actaastro.2010.05.016
Autor:
Mateen-ud-Din Qazi, He Linshu
Publikováno v:
Computer-Aided Design. 38:595-607
This paper presents a new design methodology for efficient conceptual design of complex systems involving multidisciplinary and computationally intensive analysis with large number of design variables. A nearly-orthogonal sampling of design space is
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0aed566be9f8320777fb49e68314b27c
https://doi.org/10.1016/j.cad.2006.02.001
https://doi.org/10.1016/j.cad.2006.02.001
Publikováno v:
Journal of Aerospace Technology and Management v.6 n.3 2014
Journal of Aerospace Technology and Management
Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA
Journal of Aerospace Technology and Management, Volume: 6, Issue: 3, Pages: 291-300, Published: SEP 2014
Journal of Aerospace Technology and Management
Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA
Journal of Aerospace Technology and Management, Volume: 6, Issue: 3, Pages: 291-300, Published: SEP 2014
For a small country with limited research budget and lack of advanced space technology, it is imperative to find new approaches for the development of low-cost launch vehicles (LV), which is, among all possibilities, an interesting option for rapid a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6fc3d54526b9d544c789346e9dfa3370
http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462014000300291
http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462014000300291
