Analytical solutions for the equations of motion of a space vehicle during the atmospheric re-entry phase on a 2-D trajectory

DOI10.1007/s10569-009-9199-0zbMath1223.70092OpenAlexW2018214784MaRDI QIDQ642267

Gabriel Mititelu

Publication date: 26 October 2011

Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10569-009-9199-0

zbMATH Keywords

exponential integralgeneralized exponential integralplanar motionanalytical solutions for differential equationsdynamical equations of atmospheric re-entry

Mathematics Subject Classification ID

Orbital mechanics (70M20)

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Cites Work

• Dynamics of a satellite orbiting a planet with an inhomogeneous gravitational field
• Satellites and Riemannian geometry
• Ground traces of artificial earth satellites
• SOME EXACT ANALYTICAL SOLUTIONS OF PLANETARY ENTRY
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