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Quasi-periodic orbits of the restricted three-body problem made easy
Egemen Kolemen
, N. Jeremy Kasdin
, Pini Gurfil
Mechanical & Aerospace Engineering
Andlinger Center for Energy & the Environment
Research output
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Chapter in Book/Report/Conference proceeding
›
Conference contribution
38
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Scopus citations
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Keyphrases
Restricted Three-body Problem
100%
Quasi-periodic Orbit
100%
Invariant Tori
75%
Fourier Coefficients
50%
Closed Orbits
50%
Two Dimensional
25%
Halo
25%
Execution Time
25%
Fast Execution
25%
Differential Equations
25%
Iteration Scheme
25%
Numerical Methods
25%
Libration Points
25%
Continuation Method
25%
Poincaré Map
25%
Given Accuracy
25%
Chaotic Regions
25%
Minimal Memory
25%
Invariancy
25%
Overhead Costs
25%
Lissajous
25%
Full Convergence
25%
Newton Iteration
25%
Robust Behavior
25%
Truncated Fourier Series
25%
Engineering
Body Problem
100%
Fourier Coefficient
100%
Two Dimensional
50%
Execution Time
50%
Numerical Methods
50%
Main Advantage
50%
Fourier Series
50%
Mathematics
Restricted Three-Body Problem
100%
Periodic Orbit
100%
Circle
50%
Fourier Coefficient
50%
Differential Equation
25%
Iteration Scheme
25%
Execution Time
25%
Numerical Methods
25%
Newton Iteration
25%
Poincar Map
25%
Physics
Orbit
100%
Three Body Problem
100%
Operators (Mathematics)
25%
Mathematical Method
25%
Lagrangian Points
25%