Uzair AnsariAbdulrahman H. Bajodah
This paper presents a control design approach for attitude tracking of Satellite Launch Vehicles (SLVs) based on adaptive fuzzy sliding mode control (AFSMC) with integral sliding mode switching surfaces.
Uzair AnsariAbdulrahman H. Bajodah
Wang ZhaoQing WangZhang Xin-juan
Ping GuanXiangjie LiuJizhen Liu