Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Daniel Biezad"'
Autor:
Daniel Biezad, Joon Kim
Publikováno v:
2007 Annual Conference & Exposition Proceedings.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8b11850ab1b65fc352ef0ff571b7f76f
https://doi.org/10.18260/1-2--2627
https://doi.org/10.18260/1-2--2627
Autor:
Joon Kim, Daniel Biezad
Publikováno v:
2005 Annual Conference Proceedings.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::19d60b27abfad10c185e0bafc8b02c18
https://doi.org/10.18260/1-2--15103
https://doi.org/10.18260/1-2--15103
Autor:
Jin Tso, Daniel Biezad
Publikováno v:
2001 Annual Conference Proceedings.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e56c7d29999880d94d1937d6f0c63f70
https://doi.org/10.18260/1-2--8884
https://doi.org/10.18260/1-2--8884
Autor:
Daniel Biezad
Publikováno v:
2015 ASEE Annual Conference and Exposition Proceedings.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b4bc432f899b7ba955b5714cc0d2518f
https://doi.org/10.18260/p.24021
https://doi.org/10.18260/p.24021
Publikováno v:
Modeling and Simulation Technologies Conference and Exhibit.
The simulation of modern aircraft with lightweight structures and high bandwidth control systems requires more sophisticated modeling than the standard six degree-of-freedom representation. The objective of this work was to investigate and test metho
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::91dcc04967f3c74eeacb6a600ce93987
https://doi.org/10.2514/6.1999-4320
https://doi.org/10.2514/6.1999-4320
Publikováno v:
24th Atmospheric Flight Mechanics Conference.
Large aircraf3 may possess slow structural modes that can affect handling qualities if excited Little has been done to simulate these structural modes during pilot in the loop analyses. A fast and simple method to simulate the longitudinal structural
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2cee22ce179c4824911fecb74665f330
https://doi.org/10.2514/6.1999-4108
https://doi.org/10.2514/6.1999-4108
Autor:
Mark Tischler, Jason Colbourne, Mark Morel, Daniel Biezad, William Levine, Veronica Moldoveanu
Publikováno v:
Guidance, Navigation, and Control Conference.
A state-of-the-art computational facility for aircraft flight control design, evaluation, and integration called CONDUIT (Control Designer's Unified Interface) has been developed. This paper describes the CONDUIT tool and case study applications to c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fe6bc925d26a1c1fe3f454d8b17378f0
https://doi.org/10.2514/6.1997-3773
https://doi.org/10.2514/6.1997-3773
Publikováno v:
34th Aerospace Sciences Meeting and Exhibit.
A FORTRAN computer program is presented to perform agility analysis on fighter aircraft configurations. This code is one of the modules of the NASA Ames ACSYNT (AirCraft SYNThesis) design code. The background of the agility research in the aircraft i
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::912359824a30c3cdc6a59779fd29aa96
https://doi.org/10.2514/6.1996-88
https://doi.org/10.2514/6.1996-88
Publikováno v:
32nd Aerospace Sciences Meeting and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8e8789cd4f114095d9826feb9660173e
https://doi.org/10.2514/6.1994-275
https://doi.org/10.2514/6.1994-275