Zobrazeno 1 - 1
of 1
pro vyhledávání: '"Marzieh Eghlimi Dezh"'
Publikováno v:
مکانیک هوافضا, Vol 19, Iss 1, Pp 137-151 (2023)
An active vibration control algorithm and robust integral sliding mode control (SMC) are discussed to stabilize the attitude of the flexible spacecraft under external disturbances and actuator faults. As a coupled rigid-flexible dynamical system, the
Externí odkaz:
https://doaj.org/article/6f98c4fb97764215af1ce5c429d9a0a4
