Zobrazeno 1 - 10
of 13
pro vyhledávání: '"Jennie R. Johannesen"'
Autor:
William McAlpine, Jennie R. Johannesen, Douglas Bernard, Robert D. Abelson, Laura Newlin, Try Lam
Publikováno v:
Advances in Space Research. 52:547-568
NASA’s Juno mission launched in 2011 and will explore Jupiter and its near environment starting in 2016. Planetary protection requirements for avoiding the contamination of Europa have been taken into account in the Juno mission design. In particul
Autor:
Paul K. Henry, J. Ludwinski, Stephen C. Brewster, Edward J. Jorgensen, Jennie R. Johannesen, Richard P. Kemski, K. Clark, James E. Randolph, Robert W. Maddock, John B. Carraway, J.F. Mondt, Robert L. Staehle, Alok Chatterjee, Richard J. Terrile, Richard J. Doyle, Torrence V. Johnson, Bruce T. Tsurutani
Publikováno v:
Acta Astronautica. 45:423-439
Three radii from the surface of the Sun… more natural radiation around Jupiter than would be encountered immediately following a nuclear war… to the farthest planet and beyond… these challenges are faced by the three “Ice & Fire” missions:
Publikováno v:
AIAA/AAS Astrodynamics Specialist Conference and Exhibit.
The Juno mission to Jupiter is targeted to launch in 2011 and would reach the giant planet about five years later. The interplanetary trajectory is planned to include two large deep space maneuvers and an Earth gravity assist a little more than two y
Publikováno v:
AIAA/AAS Astrodynamics Specialist Conference and Exhibit.
Juno is an orbiter mission expected to launch in 2011 to Jupiter. Juno's science orbit is a highly eccentric orbit with a period of about 11 days and a nominal duration of one year. Initially, the equatorial crossing near apojove occurs outside Calli
Autor:
Nguyen X. Vinh, Jennie R. Johannesen
Publikováno v:
Acta Astronautica. 13:291-299
This paper presents the solution for minimum-fuel, free-time transfer between coplanar elliptical orbits with the possible use of a planetary atmosphere to generate a decelerative braking force. The optimal pure propulsive two-impulse transfer is fir
Publikováno v:
Scopus-Elsevier
This paper presents the complete analysis of the problem of minimum-fuel aeroassisted transfer between coplanar elliptical orbits in the case where the orientation of the final orbit is free for selec- tion in the optimization process. The comparison
Autor:
Nguyen X. Vinh, Jennie R. Johannesen
Publikováno v:
Acta Astronautica. 12:791-802
The concept of the Darboux point at which an extremal loses its global optimality is extended to the case of discontinuous control. Using Contensou's domain of maneuverability, the condition for optimal switching at a corner is derived and the optima
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Conference
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