Difference between revisions of "Optimization of Passive Orbit with the Use of Gravity Maneuver"
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| title = Optimization of Passive Orbit with the Use of Gravity Maneuver | | title = Optimization of Passive Orbit with the Use of Gravity Maneuver | ||
| url = [http://www.naturalphilosophy.org/pdf/abstracts/abstracts_845.pdf Link to paper] | | url = [http://www.naturalphilosophy.org/pdf/abstracts/abstracts_845.pdf Link to paper] | ||
− | | author = [[Joseph J | + | | author = [[Joseph J Smulsky]] |
| keywords = [[Computing]], [[Sun system]], [[orbits]], [[spasecraft]], [[Gravity Maneuver]] | | keywords = [[Computing]], [[Sun system]], [[orbits]], [[spasecraft]], [[Gravity Maneuver]] | ||
| published = 2008 | | published = 2008 | ||
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A high-precision method of calculating gravitational interactions is applied in order to determine optimal trajectories. A number of problems, necessary for determination of optimal parameters at a launch of a spacecraft and during its flyby near celestial bodies, are considered. The spacecraft trajectory was determined by numerical integration of the equations of passive motion of the spacecraft and of the equations of motion for planets, the Sun, and the Moon. The optimal trajectory of the spacecraft approaching the Sun is determined by fitting its initial conditions. | A high-precision method of calculating gravitational interactions is applied in order to determine optimal trajectories. A number of problems, necessary for determination of optimal parameters at a launch of a spacecraft and during its flyby near celestial bodies, are considered. The spacecraft trajectory was determined by numerical integration of the equations of passive motion of the spacecraft and of the equations of motion for planets, the Sun, and the Moon. The optimal trajectory of the spacecraft approaching the Sun is determined by fitting its initial conditions. | ||
− | [[Category:Scientific Paper]] | + | [[Category:Scientific Paper|optimization passive orbit use gravity maneuver]] |
[[Category:Gravity]] | [[Category:Gravity]] |
Revision as of 10:51, 1 January 2017
Scientific Paper | |
---|---|
Title | Optimization of Passive Orbit with the Use of Gravity Maneuver |
Read in full | Link to paper |
Author(s) | Joseph J Smulsky |
Keywords | Computing, Sun system, orbits, spasecraft, Gravity Maneuver |
Published | 2008 |
Journal | Cosmic Research |
Volume | 46 |
Number | 5 |
No. of pages | 9 |
Pages | 456?464 |
Read the full paper here
Abstract
A high-precision method of calculating gravitational interactions is applied in order to determine optimal trajectories. A number of problems, necessary for determination of optimal parameters at a launch of a spacecraft and during its flyby near celestial bodies, are considered. The spacecraft trajectory was determined by numerical integration of the equations of passive motion of the spacecraft and of the equations of motion for planets, the Sun, and the Moon. The optimal trajectory of the spacecraft approaching the Sun is determined by fitting its initial conditions.