Awad, Ahmed
Wang, Haoping
Funding for this research was provided by:
National Natural Science Foundation of China (61304077)
International Science & Technology Cooperation Program of China (2015DFA01710)
Natural Science Foundation of Jiangsu Province of China (BK20130765)
Chinese Ministry of Education Project of Humanities and Social Sciences (13YJCZH171)
11th Jiangsu Province Six Talent Peaks of High Level Talents Project of China (2014_ZBZZ_005)
Jiangsu Province Project Blue: Young Academic Leaders Project
This article is maintained by: Elsevier
Article Title: Roll-pitch-yaw autopilot design for nonlinear time-varying missile using partial state observer based global fast terminal sliding mode control
Journal Title: Chinese Journal of Aeronautics
CrossRef DOI link to publisher maintained version: https://doi.org/10.1016/j.cja.2016.04.020
Content Type: article
Copyright: © 2016 Chinese Society of Aeronautics and Astronautics. Production and hosting by Elsevier Ltd.