Reentry attitude control for a reusable launch vehicle with aeroservoelastic model using type‐2 adaptive fuzzy sliding mode control
Work
Year: 2018
Type: article
Authors Qi Mao, Liqian Dou, Bailing Tian, Qun Zong
Institution Tianjin University
Cites: 43
Cited by: 19
Related to: 10
FWCI: 1.984
Citation percentile (by year/subfield): 80.64
Subfield: Control and Systems Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Funders National Natural Science Foundation of China, National Natural Science Foundation of China, National Natural Science Foundation of China, Aeronautical Science Foundation of China
Grant IDS 61873340, 61673294, 61773279, 20170748003