作者: Alejandro S. Ghersin , Ricardo S. Sánchez Peña
DOI: 10.1155/2010/463709
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摘要: A formulation of an LPV control problem with regional pole placement constraints is presented, which suitable for the application a Full Block S-Procedure. It demonstrated that improved bounds can be obtained on induced L2 norm closed loop systems, while satisfying constraints. An consisting in 6 degrees freedom (DOF) space vehicle developed as example, hardware (HIL) simulation. This shows method appealing from practical point view, considering synthesized law implemented satisfactorily standard flight systems. Conclusions remarks towards use are presented well.