Adaptive Attitude Control of Helicopter System by using Feedback Linearization Method

Adaptive Attitude Control of Helicopter System by using Feedback Linearization Method

Professor    08-7703202#7462、(L)7479    jhyang@mail.npust.edu.tw
Year2008
Author楊榮華*
Author count1
Created date2019-02-19
Author order1
Corresponding authorfalse
Publication year2008
Symposium nameCACS International Automatic Control Conferenc
Publication cityTainan, Taiwan
Publication country中華民國
Start date2008-11-22
End date2008-11-22
Review system
LanguageForeign Language