A Method for Solving the Multi-Extreme Problem of Optimizing Trajectories of a Spacecraft with an Elecrto-Jet Propulsion System’s Thrust
Crossref DOI link: https://doi.org/10.1134/S001095252003003X
Published Online: 2020-06-04
Published Print: 2020-05
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Krylov, I. V.
Text and Data Mining valid from 2020-05-01
Version of Record valid from 2020-05-01
Article History
Received: 6 November 2018
Revised: 25 February 2019
Accepted: 25 April 2019
First Online: 4 June 2020