Stability analysis and flight control design of the winged reusable launch vehicle ReFEx
Crossref DOI link: https://doi.org/10.1007/s12567-020-00319-3
Published Online: 2020-06-30
Published Print: 2021-01
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Kiehn, Daniel http://orcid.org/0000-0001-7383-0740
Text and Data Mining valid from 2020-06-30
Version of Record valid from 2020-06-30
Article History
Received: 9 January 2020
Revised: 4 May 2020
Accepted: 28 May 2020
First Online: 30 June 2020