Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Christopher M. Shearer"'
Publikováno v:
AIAA Journal. 50:2820-2833
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7173dc957d042b58416de12a9867216a
https://doi.org/10.2514/1.j051392
https://doi.org/10.2514/1.j051392
Publikováno v:
Journal of Guidance, Control, and Dynamics. 31:340-357
This paper focuses on trajectory control of the 6-DOF body flxed reference frame located on a very ∞exible aircraft. The 6-DOF equations of motion of a reference point on the aircraft are coupled with the aeroelastic equations that govern the geome
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::be35766837d7acbceb875ec2cce1fd0c
https://doi.org/10.2514/1.29335
https://doi.org/10.2514/1.29335
Publikováno v:
Journal of Aircraft. 44:1528-1545
This paper focuses on the characterization of the response of a very ∞exible aircraft in ∞ight. The 6-DOF equations of motion of a reference point on the aircraft are coupled with the aeroelastic equations that govern the geometrically nonlinear
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ddc5e182f68330d3fb7e197821efe62a
https://doi.org/10.2514/1.27606
https://doi.org/10.2514/1.27606
Autor:
Patrick Senatore, Carlos E. S. Cesnik, Nathan A Pitcher, Christopher M. Shearer, Ella M. Atkins, Weihua Su
Publikováno v:
51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 18th AIAA/ASME/AHS Adaptive Structures Conference 12th.
The University of Michigan has designed and is currently building an unmanned aerial vehicle, denoted X-HALE, which is aeroelastically representative of very flexible aircraft. The objective of this test bed is to collect unique data of the geometric
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::85dcbb44f7f37875cefc66fa619933ab
https://doi.org/10.2514/6.2010-2715
https://doi.org/10.2514/6.2010-2715
Publikováno v:
AIAA Guidance, Navigation, and Control Conference and Exhibit.
This paper focuses on trajectory control of the 6-DOF body flxed reference frame located on a very ∞exible aircraft. The 6-DOF equations of motion of a reference point on the aircraft are coupled with the aeroelastic equations that govern the geome
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bf00e6dc1bccfffde3e56efe4f282240
https://doi.org/10.2514/6.2006-6316
https://doi.org/10.2514/6.2006-6316
Publikováno v:
47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 14th AIAA/ASME/AHS Adaptive Structures Conference 7th.
This paper focuses on the time integration of the nonlinear EOM associated with a very ∞exible aircraft in ∞ight. Various integration methods exist for linear structural dynamics problems. However, a review of the literature indicates little mate
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::327b50d452787bfea0bdd59cbee57a03
https://doi.org/10.2514/6.2006-1747
https://doi.org/10.2514/6.2006-1747
