In this paper. a reaching law-based adaptive fixed-time terminal sliding mode control law. which is used for coupled spacecraft tracking maneuver in the presence of large inertia parametric uncertainties and external disturbances. is proposed. https://www.greenbeanbabyboutiques.shop/product-category/ornament/
Ornament
Internet 2 hours 16 minutes ago wuqmkic8zbgtqWeb Directory Categories
Web Directory Search
New Site Listings