Computer Science – Performance
Scientific paper
Jul 1975
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1975aiaa.conf.....u&link_type=abstract
American Astronautical Society and American Institute of Aeronautics and Astronautics, Astrodynamics Specialist Conference, Nass
Computer Science
Performance
Hyperbolic Trajectories, Jupiter (Planet), Planetary Orbits, Swingby Technique, Trajectory Optimization, Transfer Orbits, Algorithms, Elliptical Orbits, Flight Paths, Gravity Anomalies, Insertion, Io, Orbital Maneuvers, Orbital Mechanics, Orbital Velocity
Scientific paper
This paper is a description of recent studies of constrained optimal transfer between given hyperbolic asymptotes with an emphasis on the practical aspects of the concept for powered Galilean satellite swingby Jupiter orbit insertion. The effects of orbital inclination on performance gain are discussed and the targeting problem for establishing the optimal swingby is solved. Comparisons of some candidate mission profiles are presented and the advantages and disadvantages of the powered swingby orbit insertion are discussed in the context of recent interactions with the scientific community on the relative merits of several mission profiles now under consideration.
No associations
LandOfFree
The powered swingby and its application to Jupiter orbit mission design does not yet have a rating. At this time, there are no reviews or comments for this scientific paper.
If you have personal experience with The powered swingby and its application to Jupiter orbit mission design, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and The powered swingby and its application to Jupiter orbit mission design will most certainly appreciate the feedback.
Profile ID: LFWR-SCP-O-1754740