0.0 1.0 1.0 1.0    1.0 0.0   1.0 0.0   0.0 0.0     1.0     0.0     0.0
0.0 1.0 1.0 1.0    0.0 1.0   1.0 1.0   1.0 1.0     1.0     1.0     1.0

 T   P   Q   R      V  ALP   BTA THA   PSI PHI      H       X       Y

These weights specify the relative importance of state variable errors.

The angle of attack, ALP, pitch, THA, heading, PSI, bank angle, PHI,
northing, X, easting, Y, and acceleration, dV/dT, are not constrained
except they effect a coordinated turn.  There should never be any error
in the time, T, or the derivative, dT/dT.  The weights associated with
these state variables were set to zero because they have no importance.

The airspeed, V, and altitude, H, are specified by constants VSET and HSET
respectively.  The sideslip, BTA, should be zero.  The roll rate, P,
pitch rate, Q, and yaw rate, R, as well as the remaining state variables
should be kept small so that the aircraft does not maneuver too violently.
No attempt was made to distinguish the relative importance of these state
variables so the weights associated with them were arbitrarily set to one.
