Robust Controller Design of Non-minimum Phase Hypersonic Aircrafts Model based on Quantitative Feedback Theory
Crossref DOI link: https://doi.org/10.1007/s40295-019-00187-y
Published Online: 2019-07-17
Published Print: 2020-03
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Li, Zhaoying
Zhou, Wenjie
Liu, Hao http://orcid.org/0000-0001-8365-8008
Funding for this research was provided by:
National Natural Science Foundation of China (61873012)
National Natural Science Foundation of China (61503012)
Text and Data Mining valid from 2019-07-17
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Article History
First Online: 17 July 2019