Quaternion Methods and Regular Models of Celestial and Space Flight Mechanic: Using Euler (Rodrigues–Hamilton) Parameters to Describe Orbital (Trajectory) Motion. II: Perturbed Spatial Restricted Three-Body Problem
Crossref DOI link: https://doi.org/10.3103/S0025654422600787
Published Online: 2023-04-20
Published Print: 2023-02
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Chelnokov, Yu. N.
Text and Data Mining valid from 2023-02-01
Version of Record valid from 2023-02-01
Article History
Received: 29 October 2021
Revised: 13 March 2022
Accepted: 14 March 2022
First Online: 20 April 2023