Synthesis and analysis of dynamic inversion and LPV tailless flight control law designs

Modular Control Law Design for the Innovative Control Effectors (ICE) Tailless Fighter Aircraft Configuration 101-3

“…Similarly since the maximum structured singular value for robust performance is approximately 1.2 for all flight conditions, robust performance is guaranteed at all flight conditions for -^ Along. More details of this analysis, as well as a comparison with a linear parameter varying control law, appear in [9]. …”

Modular Control Design for the Innovative Control Effectors (ICE) Tailless Fighter Aircraft Configuration 101-3

“…Similarly since the maximum structured singular value for robust performance is approximately 1.2 for all flight conditions, robust performance is guaranteed at all flight conditions for ^A io71s . More details of this analysis, as well as a comparison with a linear parameter varying control law, appear in [9]. …”