Low Thrust, Minimum-Propellant Optimization for Multi-Orbit Rendezvous with Uncooperative LEO Space Debris using Indirect Methods
Christian Carone
Low Thrust, Minimum-Propellant Optimization for Multi-Orbit Rendezvous with Uncooperative LEO Space Debris using Indirect Methods.
Rel. Manuela Battipede, Luigi Mascolo. Politecnico di Torino, Master of science program in Aerospace Engineering, 2024
