Mercurial > hg > octave-terminal
changeset 3394:ef325b58db16
[project @ 1999-12-18 01:13:39 by jwe]
author | jwe |
---|---|
date | Sat, 18 Dec 1999 01:13:39 +0000 |
parents | 23502f1740a9 |
children | 202c661c53b2 |
files | scripts/control/hinfdemo.m |
diffstat | 1 files changed, 10 insertions(+), 12 deletions(-) [+] |
line wrap: on
line diff
--- a/scripts/control/hinfdemo.m +++ b/scripts/control/hinfdemo.m @@ -17,19 +17,17 @@ ## Software Foundation, 59 Temple Place, Suite 330, Boston, MA 02111 USA. ## -*- texinfo -*- -## hinfdemo H_infinity design demos for continuous SISO and MIMO -## systems and a discrete system. -## The SISO system is difficult to control because -## it is non minimum phase and unstable. The second -## design example controls the "jet707" plant, the -## 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). -## inputs: (1) thrust and (2) elevator angle -## outputs: (1) airspeed and (2) pitch angle. -## The discrete system is a stable and second order. +## @deftypefn {Function File} {} hinfdemo () ## -## +## H_infinity design demos for continuous SISO and MIMO systems and a +## discrete system. The SISO system is difficult to control because it +## is non minimum phase and unstable. The second design example +## controls the "jet707" plant, the 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). Inputs: (1) thrust and (2) elevator angle +## outputs: (1) airspeed and (2) pitch angle. The discrete system is a +## stable and second order. +## ## @table @asis ## @item SISO plant ## @display