Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Martins Sudars"'
Development and simulations of aircraft guidance system using a 3–degree‐of‐freedom point mass model
Autor:
Martins Sudars
Publikováno v:
Aviation, Vol 13, Iss 2 (2009)
Numerical simulations play an essential role in the development and testing of navigation and guidance algorithms, especially when developer must keep the development costs as low as possible. Low budget development focuses mainly on utilization of n
Externí odkaz:
https://doaj.org/article/1ffb3f33e47648fba6b643ff8fa3e1f4
Autor:
Cristina Parigini, Martins Sudars, Irene Pontijas, Riccardo Carducci, Jordi Freixa, Angelo Denaro, Salvatore Mancuso, Edmondo Bassano, Roberto Angelini, Gonzalo Blanco, Davide Bonetti, Rodrigo Haya-Ramos
Publikováno v:
Acta Astronautica. 124:39-52
The Intermediate eXperimental Vehicle (IXV) is a suborbital re-entry demonstrator successfully launched in February 2015 focusing on the in-flight demonstration of a lifting body system with active aerodynamic control surfaces. This paper presents an
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::47f214148698f392ada492ac3cdd9cf3
https://doi.org/10.1016/j.actaastro.2015.12.048
https://doi.org/10.1016/j.actaastro.2015.12.048
Autor:
Jan Thoemel, Martins Sudars, F. Ratti, Raffaele Aulisio, Thales Alenia, Jose Gavira, Gianluca Passarelli, Alvaro Martinez Barrio, Louis Walpot, Federico Massobrio
Publikováno v:
AIAA Guidance, Navigation, and Control Conference.
10 European Space Agency, ESA-ESTEC. Keplerlaan 1, Noordwijk 2200 AG, The Netherlands EXPERT is developed by the European Space Agency (ESA) and an Industrial Consortium led by Thales Alenia Space as Prime Contractor in order to provide the scientifi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9c1826fe5c162b9406543e4b1cb2e24a
https://doi.org/10.2514/6.2011-6342
https://doi.org/10.2514/6.2011-6342
Publikováno v:
20th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar.
This paper describes an approach to modeling of parachute system’s dynamics inside a synthetic flight mechanics simulation environment. Mission analysis of re-entry vehicles usually must deal with descent and landing phase. In order to evaluate the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0ba6ee3f016d2a7ed95f4c91afb57e2a
https://doi.org/10.2514/6.2009-2943
https://doi.org/10.2514/6.2009-2943
Autor:
Sudars, Martins1 msudars@yahoo.com
Publikováno v:
Aviation (1648-7788). 2009, Vol. 13 Issue 2, p35-43. 9p. 1 Color Photograph, 7 Diagrams, 15 Graphs.