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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 ~ .

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