Spacecraft-Trajectory-Design-using-Space-Manifold-Dynamics

版本 1.0.2 (3.3 MB) 作者: Arun Suresh
Low Energy trajectories
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更新时间 2023/2/26
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Low Energy trajectories that mostly utilises natural dynamics are now used to design successful and efficient missions. A single spacecraft is designed to orbit moons of Jupiter, Ganymede and Europa. The mission utilizes dynamical channels in the phase space which connects the vicinity of Ganymede to that of Europa. The system is highly nonlinear and dependent on initial condition. Dynamic equations are obtained and a controller based on the dynamic inverse is synthesized for the purpose of stabilization and trajectory tracking

引用格式

A Suresh, UP Rajeev, WC ArunKishore, "Heteroclinic Connection in Galilean Moon Orbiter Mission Using Space Manifold Dynamics," National Conference on Technological Trends, Trivandrum, Kerala, India, 2015.

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MANIFOLDS

MATLAB MANIFOLDS

PCR3BP/Earth moon/Matlab Code

PCR3BP/Jupiter Europa/Matlab Code

coordinate transformation

dynamic inversion

moon

others

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版本 已发布 发行说明
1.0.2

See release notes for this release on GitHub: https://github.com/arunsuresh990/Spacecraft-Trajectory-Design-using-Space-Manifold-Dynamics/releases/tag/V1.0.2
1.0.1

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1.0.0

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