strutLdgEdgeX strutLdgEdgeBtmZ strutChord Mass C of G(X) C of G(Z) Roll Pitch Yaw
strutSep mainFoilChord mainFoilAOfA kX (MoI) Lin. Damp X Ang. Damp X Knots Port Thrust Stbd Thrust
% %
wingLength wingChord wingDihedral kY (MoI) Lin. Damp Y Ang. Damp Y Ride Height Rud. Rake Rud. Angle
% %
wingAOfA TransomBtmX TransomBtmZ kZ (MoI) Lin. Damp Z Ang. Damp Z Climb Iter. Time Sample Time
% %
rudLdgEdgeX rudLdgEdgeBtmZ rudChord vesselLength FoilFactor StrutFactor Prop. Gain Int. Gain Deriv. Gain
rudSep rudWingLength rudWingChord DepthMin DepthZero Elev, DPSmax
propellerZ propMax

N.B. Datum point (origin) for X and Z values is the transverse axis about which the (centred) rudder rotates to control the elevator foil.