Modeling of Microaccelerations Caused by Running of Attitude-Control Engines of Spacecraft with Elastic Structural Elements
Crossref DOI link: https://doi.org/10.1007/s12217-016-9507-8
Published Online: 2016-06-07
Published Print: 2016-10
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Sedelnikov, A. V.
License valid from 2016-06-07