$${H}_{\infty }$$ Approach to Performance Analysis of Missile Control Systems with Proportional Navigation Guidance Laws
Crossref DOI link: https://doi.org/10.1007/s42835-020-00617-0
Published Online: 2021-02-01
Published Print: 2021-03
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Song, Seong-Ho https://orcid.org/0000-0003-0252-0643
Funding for this research was provided by:
Hallym University (H20200514)
Text and Data Mining valid from 2021-02-01
Version of Record valid from 2021-02-01
Article History
Received: 14 July 2020
Revised: 2 October 2020
Accepted: 24 November 2020
First Online: 1 February 2021