“…As noted in Section 2.1, ICSD method with H ∞ control of a LSS needs a LFR representation of the different mechanical subsystems, so that parametric variations can be considered in the final plant model G(s). A correct and straightforward modeling technique of a multi-body flexible spacecraft is the Two-Input Two-Output Port (TITOP) modeling technique (Perez et al, 2015a;Alazard et al, 2015;Perez et al, 2015c,b), which allows casting different structural data (Finite Element Models, geometry, flexible modes) in the state-space domain, with the added possibility of including tunable variables. In substance, the different TITOP models of the different substructures can be easily assembled through load-acceleration transmission in order to reproduce the fully assembled LSS.…”