چكيده لاتين :
An analysis of on-line tiuionomotcs robust tracking controller based on variable
structure control is presented for an aerospace iaunch. vehicle, Decentralized
sliding-mode controller is designed to achieve the decoupled asymptotic tracking
of guidance commands upon. plant unccrtainiics and external disturbances.
Development and application of the controller fOT un aerospace launch oehicle
dtlring atmospheric flighl in an erpcrimenicl setting is presented to illustrate the
perjorttuuice of the control olqoriilin, against uniid qust. and internal dynam:ics
uariaiions. The proposed sliding mode control is compared to non-linear and
time-varying gain sclieilulcd aiitopiiot arul its superior perjormomce is illustrated
by simuloiion results. Furthermore. the proposed sliding-mode controller is
convenient for irnplcm,cnt(!tion.
