Rigid Spacecraft Attitude Control Using Adaptive Non-singular Fast Terminal Sliding Mode
Crossref DOI link: https://doi.org/10.1007/s40313-014-0164-0
Published Online: 2015-01-06
Published Print: 2015-04
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Tiwari, Pyare Mohan
Janardhanan, S.
Mashuq un Nabi,
Text and Data Mining valid from 2015-01-06
