Feedback Control for Directional Rendezvous Using Constant-Magnitude Low Thrust
Year: 2024
Type: article
DOI: 10.2514/1.g008096
Authors: Shribharath Balakrishnan, Pini Gurfil
Institution: Technion – Israel Institute of Technology
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Funder: Israel Science Foundation
Award: G2342662515
OpenAlex ID: W4404764055
