LinOrbLQG:

------------------------------------------------------------------------
   Generate an LQG controller for linearized relative orbit dynamics.

   Since version 7.
------------------------------------------------------------------------
   Form:
   gK = LinOrbLQG( el, QG, RG )
------------------------------------------------------------------------

   ------
   Inputs
   ------
   gK             (:)     Controller statespace object
                             - 6 states
                             - 6 inputs     (Hills frame pos & vel)
                             - 3 outputs    (Hills frame acceleration)

   -------
   Outputs
   -------
   el            (1,6)    Orbital Elements
   QG             (1)     Scalar estimator gain (make small)
   RG             (1)     Scalar regulator gain (make big)

------------------------------------------------------------------------

Children:

Common: Classes/@statespace/and.m
Common: Classes/@statespace/close.m
Common: Classes/@statespace/connect.m
Common: Classes/@statespace/eig.m
Common: Classes/@statespace/get.m
Common: Classes/@statespace/getabcd.m
Common: Classes/@statespace/getsub.m
Common: Classes/@statespace/isempty.m
Common: Classes/@statespace/mtimes.m
Common: Classes/@statespace/plus.m
Common: Classes/@statespace/series.m
Common: Classes/@statespace/set.m
Common: Classes/@statespace/statespace.m
Common: Control/QCE
Common: Control/QCR
FormationFlying: EccDynamics/FFEccLinOrb
Orbit: RHSOrbit/LinOrb
OrbitMiniToolbox: Support/M2Nu
SC: BasicOrbit/OrbRate