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pro vyhledávání: '"Clayton C. Higginson"'
Publikováno v:
Journal of Guidance, Control, and Dynamics. 38:1573-1584
This analysis addresses the problem of constructing uncertainties in initial and final satellite orbital state vectors that are dynamically consistent in Lambert’s boundary-value problem, given uncertainties in the initial and final position vector
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0377c7401f912cbc8a7e505461218de4
https://doi.org/10.2514/1.g001019
https://doi.org/10.2514/1.g001019
