Report of the Second Piloted Aircraft Flight Control System - Acgsc.org
Report of the Second Piloted Aircraft Flight Control System - Acgsc.org
Report of the Second Piloted Aircraft Flight Control System - Acgsc.org
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f<br />
Ewr valve neutral, vita 4 =O , <strong>the</strong> open tranrf er<br />
function becaes simple, since cF r O o (See Fig. 4.) Haling<br />
tM8 abstitution plus <strong>the</strong> nlationship 4 = A W 'r<br />
(<strong>the</strong> effective spring due ta oil ~ressibillty),<br />
equation (a) bemar:<br />
Eqrrgtion (25), though representative <strong>of</strong> a rirpllfied mtem, is<br />
still quite qlex. It is <strong>the</strong>refore <strong>of</strong> considerable ralue to attrpt<br />
approximate factarieation, and to consider Uniting case80<br />
Equations (24) and (25) are <strong>of</strong> <strong>the</strong> forp<br />
as- that <strong>the</strong> denabator frequencier are wldely separated, it is<br />
possible to obtain an'appmxbate factorisation <strong>of</strong> <strong>the</strong> donainator In<br />
eneral torrs0 (See Table I,) The mathod originally developed by Lin<br />
f<br />
Refemc9 2) is enplopd for <strong>the</strong> factor is at ion^ it is asmod tbt <strong>the</strong><br />
first trial solution wnvdrges ianediately, In this situation, <strong>the</strong> Bode<br />
diagrerp <strong>of</strong> <strong>the</strong> rhplUi4 syat~l will appear as r h in Pig, 8, k-<br />
prlmental point8 are plotted os top <strong>of</strong> <strong>the</strong> calculated valuer for a ttpid<br />
p ~ i ~ s y 8 t ~ .