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ASE 388P.2

Celestial Mechanics I

The University of Texas at Austin 3 credits Aerospace Engineering

Course Description

N-body problem; three-body problem; restricted three-body problem; Jacobian integral; zero-velocity curves; equilibrium points; stability; linearized solutions; variational equations; periodic orbits; the two-body problem; variation of parameters; Lagrange's planetary equations; applications to near-earth and deep-space trajectories; numerical methods.

Code
ASE 388P.2
Credits
3
Subject
Aerospace Engineering

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