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Firstly, the model of HV is transformed into two strict feedback subsystem: the mismatched subsystem of altitude and the matched subsystem of velocity. Then, the TSMC and back-stepping method is incorporated to cope with the unmatched issue in the HV altitude subsystem. In addition, a NDO based on a finite-time-convergent differentiator (FD) is proposed to estimate the lumped disturbances. The finite-time stability condition of the system is established via the Lyapunov theory. Finally, the robustness and effectiveness of the method are verified by simulations.<\/jats:p>","DOI":"10.1177\/0142331219857301","type":"journal-article","created":{"date-parts":[[2019,6,24]],"date-time":"2019-06-24T09:57:00Z","timestamp":1561370220000},"page":"4339-4350","update-policy":"https:\/\/doi.org\/10.1177\/sage-journals-update-policy","source":"Crossref","is-referenced-by-count":16,"title":["A finite-time sliding mode control for hypersonic vehicle"],"prefix":"10.1177","volume":"41","author":[{"given":"Qingwen","family":"Ma","sequence":"first","affiliation":[{"name":"Institute of Precision Guidance and Control, Northwestern Polytechnical University, P.R.China"}],"role":[{"role":"author","vocabulary":"crossref"}]},{"given":"Jianguo","family":"Guo","sequence":"additional","affiliation":[{"name":"Institute of Precision Guidance and Control, Northwestern Polytechnical University, 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