Composite Design of Disturbance Observer and Reentry Attitude Controller: An Enhanced Finite-time Technique for Aeroservoelastic Reusable Launch Vehicles
Crossref DOI link: https://doi.org/10.1007/s12555-021-0643-6
Published Online: 2022-07-12
Published Print: 2022-08
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Yang, Zhenshu
Mao, Qi http://orcid.org/0000-0001-8513-5577
Dou, Liqian
Zong, Qun
Yang, Jianzhong
Text and Data Mining valid from 2022-07-12
Version of Record valid from 2022-07-12
Article History
Received: 4 August 2021
Revised: 24 September 2021
Accepted: 7 October 2021
First Online: 12 July 2022