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Autor:
Marco Sagliano, José V. Garrido
This paper illustrates the trajectory modeling of multistage rockets for both ascent anddescent phases. The computation of solutions is performed by coupling a multiphase optimal-control problem formulation with a transcription performed via Radau ps
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::0d3c01efe48a90b4bef0f51d8a20a20a
https://elib.dlr.de/140558/
https://elib.dlr.de/140558/
