An Analytical Solution to the Problem of Optimal Control of the Reorientation of a Rigid Body (Spacecraft) Using Quaternions
Crossref DOI link: https://doi.org/10.3103/S002565441907001X
Published Online: 2020-04-20
Published Print: 2019-12
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Levskii, M. V.
Text and Data Mining valid from 2019-12-01
Version of Record valid from 2019-12-01
Article History
Received: 22 November 2018
Revised: 22 November 2018
Accepted: 19 December 2018
First Online: 20 April 2020