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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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The error equation (l), with XI * ir, R b-es<br />

also, since <strong>the</strong> piston displacrnmt Xf<br />

quation (1Ba) becmes<br />

is ngn-drtant, tho n9r<br />

The flow .quation8 (4b) (page 7 ) and (Ua') cabhe to form <strong>the</strong><br />

qrerrion<br />

The sipaplified load systm~ is rrav camplete3J defined<br />

(21) throggh (231,<br />

aquationo<br />

It now becomes a rimple algebreic task to combine equatiOIU (21)<br />

throu& (23) into <strong>the</strong> opa~ loap transfor funetian <strong>of</strong> <strong>the</strong> r;ystr.<br />

definition, <strong>the</strong> open loop transfer fmction 3npUes that all artrmeou<br />

inpats, or dirturbances, are %em; hmce <strong>the</strong> aemdpamic feree F ef<br />

equation (18) is sera.

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