Stability Margin and Structural Coupling Analysis of a Hybrid INDI Control for the Fighter Aircraft
Crossref DOI link: https://doi.org/10.1007/s42405-021-00394-8
Published Online: 2021-07-21
Published Print: 2021-10
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Kim, Chong-Sup http://orcid.org/0000-0001-5727-6030
Ji, Chang-Ho
Koh, Gi-Oak
Kim, Byoung Soo
Text and Data Mining valid from 2021-07-21
Version of Record valid from 2021-07-21
Article History
Received: 18 December 2020
Revised: 6 May 2021
Accepted: 3 June 2021
First Online: 21 July 2021
Declarations
:
: The authors declare that there is no conflict of interest regarding the publication of this paper.