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math.OC2025
Classification and Feasibility Assessment of Infinitely Many Iso-Impulse Three-Dimensional Trajectories
Keziban Saloglu, Ehsan Taheri
In two-body dynamics, it is proven that for a sufficiently long flight time, generating infinitely many iso-impulse solutions is possible by solving a number of -allocation pr…
math.OC2024
Co-optimization of spacecraft and low-thrust trajectory with direct methods
Keziban Saloglu, Ehsan Taheri
Solar-powered electric propulsion systems can operate in multiple modes and their operation is coupled to the power generated by solar arrays. However, the power produced by the so…