2026-09-25T08:16:12Zhttps://iris.polito.it/oai/requestoai:iris.polito.it:11583/29765952023-06-30T08:55:37Zcom_11583_2614433com_11583_2614425col_11583_2614423
Low-Thrust Optimal Escape Trajectories from Lagrangian Points and Quasi-Periodic Orbits in a High-Fidelity Model
MASCOLO, LUIGI
Mascolo, Luigi
CASALINO, LORENZO
Escape Trajectorie
Lagrangian Point
Electric Propulsion
Trajectory Optimization
Indirect Method
Earth-Moon
Sun-Earth
Quasi-Periodic Orbit
Higher Fidelity Model
Optimal Control
Autonomous Solution Search
Settore ING-IND/07 - Propulsione Aerospaziale
L'abstract è presente nell'allegato / the abstract is in the attachment
2023-02-03
info:eu-repo/semantics/doctoralThesis
https://hdl.handle.net/11583/2976595
eng
firstpage:1
lastpage:217
numberofpages:217
info:eu-repo/semantics/openAccess
Politecnico di Torino
country:Italy
license:Creative commons
license:Creative commons
license uri:http://creativecommons.org/licenses/by-nc-nd/4.0/
license uri:http://creativecommons.org/licenses/by-nc-nd/4.0/