Spacecraft Attitude Maneuver Using Fast Terminal Sliding Mode Control Based on Variable Exponential Reaching Law
Crossref DOI link: https://doi.org/10.1007/978-981-15-1773-0_1
Published Online: 2020-03-01
Published Print: 2020
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Wu, Yue-Dong
Wu, Shu-Fan
Gong, De-Ren
Kang, Ze-Yu
Wang, Xiao-Liang
Text and Data Mining valid from 2020-01-01
Version of Record valid from 2020-01-01
Chapter History
First Online: 1 March 2020