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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CHART ILLUSTRATING EFFECT OF INERTIA INDEX E<br />
ON SERVOMOTOR SIZE<br />
FIGURE 10<br />
CONCLUDING l3mARKs<br />
The discussion has shown that <strong>the</strong> response characteristics <strong>of</strong><br />
hydraulic servomotors with mechanical feedback may be represented by linear<br />
equations. These equations are defined in terms <strong>of</strong> <strong>the</strong> size <strong>of</strong> <strong>the</strong><br />
servomotor and <strong>the</strong> load conditions. From <strong>the</strong>se relations, equations which<br />
define <strong>the</strong> dimensions <strong>of</strong> <strong>the</strong> servomotor i n terms <strong>of</strong> <strong>the</strong> known load, and<br />
desired response characteristics can be obtained. BY means <strong>of</strong> <strong>the</strong>se relations<br />
<strong>the</strong> rational design <strong>of</strong> <strong>the</strong> servomotor to meet specifications on<br />
ei<strong>the</strong>r <strong>the</strong> transient or frequency response characteristics is made<br />
possible.<br />
1. W A <strong>Report</strong>. Dynamics <strong>of</strong> Mechanical Feedback-Type .Hydraulic Servomotor<br />
under Inertia Loads, by Harold Gold; Edward W. Otto, and<br />
Victor L. Ransom (soon to be published) .
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