摘要：A formulation of an LPV control problem with regional pole placement constraints is presented,
which is suitable for the application of a Full Block S-Procedure. It is demonstrated that improved
bounds can be obtained on the induced 𝐿2 norm of closed loop systems, while satisfying pole placement
constraints. An application consisting in the 6 degrees of freedom (DOF) control of a space vehicle is
developed as an example, with hardware in the loop (HIL) simulation. This shows that the method is
appealing from the practical point of view, considering that the synthesized control law can be implemented
satisfactorily in standard flight control systems. Conclusions with remarks towards the practical use of
the method are presented as well.
