roulishollandais,
Originally Posted by Cranfield, report n°9303
The application of a C* flight controllaw to large civil transport aircraft
c*= Knz.nz + Kq.q (2)
qSS=nz.g/V (4)
if Knz is set equal to 1, (...):
Kq=Vco/g (6)
If Knz is not set equal to 1, equation (6) reads:
Kq/Knz=Vco/g
V in equation (4) and Vco in equation (6) are not airspeeds but are kinematic speeds. Equation (4) applies equally in space without air, usually written as an=ω*V, for any body moving along a curved path and maintaining its orientation relative to the direction of movement.