This chapter contains sections titled:
Introduction
The Two‐body Problem—Particle Dynamics
Specifying the Orbit
Orbit Perturbations
Restricted Three‐body Problem
Celestial Mechanics
Spacecraft Systems Engineering ; 79-110
12.08.2011
32 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
hyperbolic trajectory , atmospheric drag ‐ for low Earth‐orbiting spacecraft , two‐body problem—particle dynamics ‐ motion of two co‐rotating point masses , celestial mechanics ‐ and theory, spacecraft's orbital motion , mutual gravitational force of attraction ‐ between any two bodies , Kepler's equation, simple relationship ‐ time and position , solar radiation pressure (SRP) perturbations , theory of celestial mechanics ‐ motion of a spacecraft prediction , orbit perturbations on space vehicles ‐ not included in Keplerian formulation
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