Výsledky vyhledávání - "Eugene Bonfiglio"

Mars InSight Entry, Descent, and Landing Trajectory and Atmosphere Reconstruction

Autor: David M. Kass, Ashley M. Korzun, Christopher D. Karlgaard, Mark Schoenenberger, Eugene Bonfiglio, Myron R. Grover

Publikováno v: Journal of Spacecraft and Rockets. 58:865-878

The InSight mission landed on the surface of Mars on 26 November 2018. The InSight system performance met all design requirements, although several performance metrics fell near the boundaries of t...

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6dc840aa9cc2a5fbeffc899097f617a7
https://doi.org/10.2514/1.a34913

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DSENDS: Multi-mission Flight Dynamics Simulator for NASA Missions

Autor: Jonathan M. Cameron, Abhinandan Jain, Paul D. Burkhart, Erik S. Bailey, Bob Balaram, Eugene Bonfiglio, Mark Ivanov, Joel Benito, Evgeniy Sklyanskiy, William Strauss

Publikováno v: AIAA SPACE 2016.

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::097601d2a506ae0b8757e4a3a273951f
https://doi.org/10.2514/6.2016-5421

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Automated Design of Aerogravity-Assist Trajectories

Autor: James M. Longuski, Eugene Bonfiglio, Nguyen X. Vinh

Publikováno v: Journal of Spacecraft and Rockets. 37:768-775

Aerogravity assist enhances the technique of gravity assist through the use of a lifting vehicle that ies through the atmosphere of the swingby planet. An algorithm is developed that automatically searches for such trajectories to destination plan

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::42c209845419b04baa939a0f7cad7f60
https://doi.org/10.2514/2.3649

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Navigation Challenges of the Mars Phoenix Lander Mission

Autor: Eugene Bonfiglio, Gerhard Kruizinga, Brian Portock, Mark Ryne, Behzad Raofi

Publikováno v: AIAA/AAS Astrodynamics Specialist Conference and Exhibit.

The Mars Phoenix Lander mission was launched on August 4th, 2007. To land safely at the desired landing location on the Mars surface, the spacecraft trajectory had to be controlled to a set of stringent atmospheric entry and landing conditions. The l

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::1fb73e8f59e0c5659ef7edc26fbd6c33
https://doi.org/10.2514/6.2008-7214

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Spitzer Space Telescope mission design

Autor: Stacia M. Long, Eugene Bonfiglio, Johnny H. Kwok, Mark D. Garcia

Publikováno v: SPIE Proceedings.

This paper gives a description of the mission design, launch, orbit, and navigation results for the Spitzer space telescope mission. The Spitzer telescope was launched by the Delta II Heavy launch vehicle into a heliocentric Earth trailing orbit. Thi

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::54aa0becf47c2518834901f6332f19bc
https://doi.org/10.1117/12.551598

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Trajectories to Jupiter via gravity assists from Venus, Earth, and Mars

Autor: James M. Longuski, Eugene Bonfiglio, Anastassios E. Petropoulos

Publikováno v: AIAA/AAS Astrodynamics Specialist Conference and Exhibit.

Gravity-assist trajectories to Jupiter, launching between 1999 and 2031, are identi ed using patched-conic techniques. The classical trajectories, such as the Venus–Earth–Earth gravity assist, and many less conventional paths, such as Venus–M

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c46906b69a43fdf54dbc89637d02c61f
https://doi.org/10.2514/6.1998-4284

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