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comparison scripts/control/system/jet707.m @ 5016:bdbee5282954

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[project @ 2004-09-22 02:50:35 by jwe]
author jwe
date Wed, 22 Sep 2004 02:50:36 +0000
parents b8105302cfe8
children c08cb1098afc
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5015:6d481b6e349e 5016:bdbee5282954
15 ## You should have received a copy of the GNU General Public License 15 ## You should have received a copy of the GNU General Public License
16 ## along with Octave; see the file COPYING. If not, write to the Free 16 ## along with Octave; see the file COPYING. If not, write to the Free
17 ## Software Foundation, 59 Temple Place, Suite 330, Boston, MA 02111 USA. 17 ## Software Foundation, 59 Temple Place, Suite 330, Boston, MA 02111 USA.
18 18
19 ## -*- texinfo -*- 19 ## -*- texinfo -*-
20 ## @deftypefn {Function File} {} jet707 () 20 ## @deftypefn {Function File} {@var{sys} =} jet707 ()
21 ## Creates linearized state space model of a Boeing 707-321 aircraft 21 ## Creates a linearized state-space model of a Boeing 707-321 aircraft
22 ## at v=80m/s. (M = 0.26, Ga0 = -3 deg, alpha0 = 4 deg, kappa = 50 deg) 22 ## at @var{v}=80 m/s
23 ## System inputs: (1) thrust and (2) elevator angle 23 ## @iftex
24 ## System outputs: (1) airspeed and (2) pitch angle 24 ## @tex
25 ## Ref: R. Brockhaus: Flugregelung (Flight Control), Springer, 1994 25 ## ($M = 0.26$, $G_{a0} = -3^{\circ}$, ${\alpha}_0 = 4^{\circ}$, ${\kappa}= 50^{\circ}$).
26 ## @end tex
27 ## @end iftex
28 ## @ifinfo
29 ## (@var{M} = 0.26, @var{Ga0} = -3 deg, @var{alpha0} = 4 deg, @var{kappa} = 50 deg).
30 ## @end ifinfo
31 ##
32 ## System inputs: (1) thrust and (2) elevator angle.
33 ##
34 ## System outputs: (1) airspeed and (2) pitch angle.
35 ##
36 ## @strong{Reference}: R. Brockhaus: @cite{Flugregelung} (Flight Control), Springer, 1994.
26 ## @end deftypefn 37 ## @end deftypefn
27 ## @seealso{ord2} 38 ## @seealso{ord2}
28 39
29 ## Author: Kai P. Mueller <mueller@ifr.ing.tu-bs.de> 40 ## Author: Kai P. Mueller <mueller@ifr.ing.tu-bs.de>
30 ## Created: September 28, 1997 41 ## Created: September 28, 1997