A Control Law Design Method Facilitating Control Power, Robustness, Agility, and Flying Qualities Tradeoffs: CRAFT
National Aeronautics and Space Administration, Langley Research Center, 1998 - 44 pages
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achievable eigenspace achievable eigenvectors agility metric angle of attack axis bank Closed-Loop Eigenspace Closed-Loop Eigenvectors closed-loop system contour control design metrics control input control law design control power metric CRAFT design damping ratio define Design Method design objective area design point design process designer's desirable regions Desired Closed-Loop desired eigenspace desired eigenvectors desired-model eigenvectors determined Dutch roll frequency Dutch roll mode dynamics eigenvalues and eigenvectors eigenvector design eigenvector specification equation feedback gains fighter aircraft final design flying qualities metrics flying qualities specifications frequency and damping gain magnitudes HARV Langley Research Center lateral-directional Level 1 flying McDonnell Aircraft metric surfaces metric values Mil-Std Minimum-Specification Eigenvectors mode Roll mode mode Spiral mode open-loop eigenvectors outputs pole location Pseudo Controls rate rad/sec robustness metric roll mode Roll Roll mode Spiral sideslip angle stability-axis state-space system matrix target pole thrust vectoring transfer function transformation yaw rate