Zobrazeno 1 - 10
of 39
pro vyhledávání: '"Maj Mirmirani"'
Publikováno v:
Journal of Aircraft. 46:800-813
A nonlinear wind-tunnel and computational-fluid-dynamics-based model of the longitudinal and lateral-directional dynamics for an airbreathing generic hypersonic vehicle is developed. The equations of motion for the generic hypersonic vehicle are deri
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d24bd29b03ae273174a303e1fe2b816c
https://doi.org/10.2514/1.35644
https://doi.org/10.2514/1.35644
Autor:
Zachary Kern, Richard J. Prazenica, Alfonso Noriega, Vinod Gehlot, Richard Anderson, Brandon Burnett, Maj Mirmirani, Hever Moncayo
Publikováno v:
AIAA Infotech @ Aerospace.
The integration of UAS into the National Airspace, although imminent, still presents several technological challenges. Before a sucessful integration can occur, it is necessary to demonstrate different technologies in traffic detection, traffic avoid
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3baeb3ff24326d4bf1be267962804f26
https://doi.org/10.2514/6.2015-0485
https://doi.org/10.2514/6.2015-0485
Publikováno v:
Journal of Guidance, Control, and Dynamics. 27:829-838
A multi-input/multi-output adaptive sliding controller is designed and analyzed for the longitudinal dynamics of a generic hypersonic air vehicle. This vehicle model is nonlinear, multivariable, and unstable and includes uncertain parameters. Simulat
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::18d15316b88993045e49da1a1cea39c5
https://doi.org/10.2514/1.12596
https://doi.org/10.2514/1.12596
Publikováno v:
IFAC Proceedings Volumes. 37:559-564
A key issue in making air-breathing hypersonic flight feasible and efficient is the control design. The unique dynamic characteristics of air-breathing hypersonic flight vehicles together with the aerodynamic effects of hypersonic flight make this is
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0f467dcc1f629d7458a557a7f3d4b1d0
https://doi.org/10.1016/s1474-6670(17)32234-6
https://doi.org/10.1016/s1474-6670(17)32234-6
Publikováno v:
IFAC Proceedings Volumes. 36:487-492
The design of stabilizing controllers for multi-input multi-output (MIMO) nonlinear plants with unknown nonlinearities is a challenging problem. The inability to identify the nonlinearities on-line or off-line accurately motivates the design of stabi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bf2ef11bd43634f2437e7f51f16fee33
https://doi.org/10.1016/s1474-6670(17)35711-7
https://doi.org/10.1016/s1474-6670(17)35711-7
Publikováno v:
IFAC Proceedings Volumes. 34:121-126
A robust adaptive control algorithm is proposed for a class of single-input, single-output nonlinear systems with unknown dynamics. The nonlinearities depend linearly on unknown parameters with known basis functions. It is shown that if the system sa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::36840c45c05329dce445002e77496bee
https://doi.org/10.1016/s1474-6670(17)35160-1
https://doi.org/10.1016/s1474-6670(17)35160-1
Publikováno v:
52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
Preliminary baseline finite element (FE) model calibrations and evaluations are developed to assist and guide multidisciplinary design optimization (MDO) of a large-scale hybrid composite wind turbine blade. The weight, displacement, and failure inde
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::92c184310a9a07c13257ac1c7e049dfe
https://doi.org/10.2514/6.2011-1902
https://doi.org/10.2514/6.2011-1902
Publikováno v:
ASME 2011 International Manufacturing Science and Engineering Conference, Volume 2.
A multidisciplinary design optimization (MDO) process of a large scale hybrid composite wind turbine blade is developed. Multiple objectives are considered in this design optimization: maximize length of blade, minimize weight and manufacturing cost.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7e8137c1fc202575223aff2fa7ac49a7
https://doi.org/10.1115/msec2011-50204
https://doi.org/10.1115/msec2011-50204
Publikováno v:
ACC
Flight dynamic characteristics of scramjet-powered hypersonic air vehicles are unique and have major differences with those of a conventional aircraft. These special characteristics are due to the tightly integrated engine-airframe lifting body - an
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::803ec91f8b7e1a9df81a2b27f27a958a
https://doi.org/10.1109/acc.2009.5160500
https://doi.org/10.1109/acc.2009.5160500
Publikováno v:
AIAA Guidance, Navigation and Control Conference and Exhibit.
This paper presents an adaptive mode suppression scheme that is simulated on a longitudinal model of a generic airbreathing hypersonic flight vehicle. An aerodynamically optimized vehicle model is used which has a long slender configuration and flexi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::51930d36456373d29d3da14decb21894
https://doi.org/10.2514/6.2008-7137
https://doi.org/10.2514/6.2008-7137