z-logo
open-access-imgOpen Access
Artificial Equilibrium Points in the Low-Thrust Restricted Three-Body Problem When Both the Primaries Are Oblate Spheroids
Author(s) -
Amit Mittal,
Krishan Pal
Publication year - 2018
Publication title -
international journal of astronomy and astrophysics
Language(s) - English
Resource type - Journals
eISSN - 2161-4725
pISSN - 2161-4717
DOI - 10.4236/ijaa.2018.84028
Subject(s) - physics , thrust , equilibrium point , acceleration , spacecraft , classical mechanics , stability (learning theory) , oblate spheroid , gravitation , mechanics , point (geometry) , motion (physics) , geometry , quantum mechanics , thermodynamics , astronomy , computer science , differential equation , mathematics , machine learning

The content you want is available to Zendy users.

Already have an account? Click here to sign in.
Having issues? You can contact us here
Accelerating Research

Address

John Eccles House
Robert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom