Mercurial > hg > octave-lyh
diff scripts/control/system/jet707.m @ 5016:bdbee5282954
[project @ 2004-09-22 02:50:35 by jwe]
author | jwe |
---|---|
date | Wed, 22 Sep 2004 02:50:36 +0000 |
parents | b8105302cfe8 |
children | c08cb1098afc |
line wrap: on
line diff
--- a/scripts/control/system/jet707.m +++ b/scripts/control/system/jet707.m @@ -17,12 +17,23 @@ ## Software Foundation, 59 Temple Place, Suite 330, Boston, MA 02111 USA. ## -*- texinfo -*- -## @deftypefn {Function File} {} jet707 () -## Creates linearized state space model of a Boeing 707-321 aircraft -## at v=80m/s. (M = 0.26, Ga0 = -3 deg, alpha0 = 4 deg, kappa = 50 deg) -## System inputs: (1) thrust and (2) elevator angle -## System outputs: (1) airspeed and (2) pitch angle -## Ref: R. Brockhaus: Flugregelung (Flight Control), Springer, 1994 +## @deftypefn {Function File} {@var{sys} =} jet707 () +## Creates a linearized state-space model of a Boeing 707-321 aircraft +## at @var{v}=80 m/s +## @iftex +## @tex +## ($M = 0.26$, $G_{a0} = -3^{\circ}$, ${\alpha}_0 = 4^{\circ}$, ${\kappa}= 50^{\circ}$). +## @end tex +## @end iftex +## @ifinfo +## (@var{M} = 0.26, @var{Ga0} = -3 deg, @var{alpha0} = 4 deg, @var{kappa} = 50 deg). +## @end ifinfo +## +## System inputs: (1) thrust and (2) elevator angle. +## +## System outputs: (1) airspeed and (2) pitch angle. +## +## @strong{Reference}: R. Brockhaus: @cite{Flugregelung} (Flight Control), Springer, 1994. ## @end deftypefn ## @seealso{ord2}