Control of Spacecraft and Aircraft: P10_2_2.m - File Exchange

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Highlights from
Control of Spacecraft and Aircraft

[FD,GD,AD,ND,BD]=cvrt(F,G,A,N...
[FD,GD,AD,ND,BD]=cvrt(F,G,A,N...
[FD,GD,SC,RMSY,RMSU,EV]=mimod... Table D.5; synthesizes discrete MIMO LQG prediction-compensator and
[Phi,W]=cvrtq(F,Ga,Q,T) ... Determines covariance W of full-rank random sequence wd(k) that is
[Sc,rmsy,rmsu,ev]=mimocomy(S,... Synthesizes continuous MIMO LQG compensator & determines RMS response
[XX,UX,XU,UU]=modfol(F,G,H,L,... Computes feedforward gains xx and ux for asymptotic model-following or
[y,s]=figf_4(s,A) ... Root locus vs. A for infinite-dimensional LQR for stabilizing
[y,y1,u]=stepcmd(F,G,H,L,C,yc...
s1=figf_5(s,A) ... Root locus vs. A for infinite-dimensional LQR for stabilizing
sp=loc_cap(t,s,flg,F,G,K)
zohplot(xord,yord,plotchar) ZOHPLOT Plots the zero-order hold of two columns of data.
Fig03_9.m
Fig13_25a.m
P10_2_2.m
P14_4_1a.m
P14_4_1b.m
Tab10_1.m
Tab10_2.m
Tab12_2.m
Tab12_3.m
Tab12_4.m
Tab12_5.m
Tab12_6.m
TabD_1.m
TabD_3.m
fig12_30old.m
View all files

from Control of Spacecraft and Aircraft by Arthur Bryson
Companion Software

P10_2_2.m

% Script p10_2_2.m; eigensystem for 747 longitudinal motions in 
% landing configuration; x=[du dw q dth]'; units ft, sec, crad;
%                                                         5/96, 2/1/01
%
A=[-.021 .122 0 -.322; -.209 -.530 2.21 0; .017 -1.64 -.412 0; ...
   0 0 1 0]; [V,E]=eig(A)

Highlights from Control of Spacecraft and Aircraft

Highlights from
Control of Spacecraft and Aircraft