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The trajectories of a spaceprobe ejected from a space station in circular orbit

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Publication:3051472
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DOI10.1007/BF01230406zbMath0415.70038MaRDI QIDQ3051472

T. F. Berreen

Publication date: 1979

Published in: Celestial Mechanics (Search for Journal in Brave)


zbMATH Keywords

orbital mechanicscircular orbitspace stationtrajectories of a spaceprobe


Mathematics Subject Classification ID

Orbital mechanics (70M20)


Related Items (1)

Approximate solutions of non-linear circular orbit relative motion in curvilinear coordinates



Cites Work

  • An exact and a new first-order solution for the relative trajectories of a probe ejected from a space station
  • Second-order solution to the elliptical rendezvous problem.
  • Relative motion of near orbiting satellites
  • RELATIVE TRAJECTORIES OF OBJECTS EJECTED FROM A NEAR SATELLITE


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