article · German

Zur numerischen Lösung von Randwertaufgaben des eingeschränkten Dreikörperproblems

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A two-page offprint (Sonderdruck) from Luftfahrttechnik Raumfahrttechnik (Vol. 14, 1968, pp. 220–221) presenting a numerical method for solving boundary value problems in the restricted three-body problem (Earth–Moon–spacecraft). The authors use the AEG-Telefunken Rechenanlage BA 741 analog computer to compute minimum-flight-time trajectories for an infinitesimal body (spacecraft) between two circular orbits in the rotating coordinate frame. Two distinct trajectory solutions are found and illustrated graphically.

Manufacturer: Telefunken
System: Rechenanlage BA 741
Year: 1968
Type: article
Language: German
Learning track: specific applications
Pages: 2
Author: Kurt Riedorff, Helmut Altmann

three-body problemboundary value problemsorbital mechanicsnumerical methods

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