Quaternion Methods and Regular Models of Celestial Mechanics and Space Flight Mechanics: The Use of Euler (Rodrigues–hamilton) Parameters to Describe Orbital (Trajectory) Motion. I: Review and Analysis of Methods and Models and Their Applications
Crossref DOI link: https://doi.org/10.3103/S0025654422050041
Published Online: 2022-08-25
Published Print: 2022-10
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Chelnokov, Yu. N.
Text and Data Mining valid from 2022-08-25
Version of Record valid from 2022-08-25
Article History
Received: 14 October 2021
Revised: 5 December 2021
Accepted: 7 December 2021
First Online: 25 August 2022