Nonlinear high-fidelity modeling of spacecraft relative motion via orbit element differences

Autor:	Ayansola D. Ogundele, Olufemi A. Agboola, Olasunkanmi F. Oseni
Rok vydání:	2022
Předmět:	Space and Planetary Science Control and Systems Engineering Mechanical Engineering Aerospace Engineering Computers in Earth Sciences Social Sciences (miscellaneous)
Zdroj:	Aerospace Systems. 5:591-605
ISSN:	2523-3955 2523-3947
DOI:	10.1007/s42401-022-00155-9
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::8035f98ac600f5e92f9b559ca183e618 https://doi.org/10.1007/s42401-022-00155-9 Zobrazit plný text záznamu Full text from SpringerLink