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The Art of the Helicopter John Watkinson - Karatunov.net

The Art of the Helicopter John Watkinson - Karatunov.net

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7.1 Introduction<br />

7<br />

Control<br />

<strong>The</strong> physical control requirement in a helicopter is no more than <strong>the</strong> application <strong>of</strong><br />

appropriate cyclic, collective and tail rotor pitch settings. Implicit in this is <strong>the</strong> need for<br />

some form <strong>of</strong> rotor speed governing. However, <strong>the</strong> physical control requirement is only<br />

a small part <strong>of</strong> <strong>the</strong> overall process that is inevitably more complex. In order to perform<br />

useful missions in safety, <strong>the</strong> pitch settings <strong>of</strong> <strong>the</strong> rotors must be such that at all times<br />

<strong>the</strong> machine has, for example, <strong>the</strong> desired attitude, airspeed, altitude and geographical<br />

location.<br />

In order to control <strong>the</strong> flight, information must be ga<strong>the</strong>red about <strong>the</strong> present conditions,<br />

and <strong>the</strong>se must be compared with <strong>the</strong> desired conditions. Any discrepancies must<br />

result in changes to <strong>the</strong> physical controls that would tend to reduce discrepancies to<br />

zero or at least as near as makes no difference. This is, <strong>of</strong> course, classical negative feedback<br />

as was introduced in Chapter 2. <strong>The</strong> essential components <strong>of</strong> this process must<br />

be information ga<strong>the</strong>ring, or sensing, information transmission, decision-making, or<br />

information processing, all <strong>of</strong> which takes place with small amounts <strong>of</strong> power, followed<br />

by a power amplification stage that allows <strong>the</strong> control information actually to operate<br />

<strong>the</strong> controls.<br />

Figure 7.1(a) shows <strong>the</strong> case <strong>of</strong> a simple light helicopter. It will have instruments<br />

such as airspeed indicator, altimeter and compass whose output is purely visual. <strong>The</strong><br />

pilot looks at <strong>the</strong> instruments and out <strong>of</strong> <strong>the</strong> canopy in order to establish <strong>the</strong> actual<br />

conditions, but has to perform all <strong>of</strong> <strong>the</strong> actions necessary to stabilize <strong>the</strong> machine and<br />

hold it on a desired course. <strong>The</strong> machine itself may actually be unstable, in that left to<br />

itself it would diverge from its original course, but <strong>the</strong> combination <strong>of</strong> <strong>the</strong> pilot and <strong>the</strong><br />

machine can be a stable system. In o<strong>the</strong>r words <strong>the</strong> pilot is working out <strong>the</strong> difference<br />

between what is wanted and what is actually happening. As a result <strong>of</strong> a difference<br />

<strong>of</strong> this kind <strong>the</strong> pilot <strong>the</strong>n has to operate one or more <strong>of</strong> <strong>the</strong> controls in a sense that<br />

reduces <strong>the</strong> difference. An unskilled pilot may overcontrol so that <strong>the</strong> machine oscillates<br />

about <strong>the</strong> desired course, whereas <strong>the</strong> experienced pilot will have learned <strong>the</strong> dynamics<br />

<strong>of</strong> <strong>the</strong> machine and applies just <strong>the</strong> right control inputs smoothly to bring <strong>the</strong> difference<br />

to zero.<br />

In Figure 7.1(a) <strong>the</strong> pilot is part <strong>of</strong> a feedback loop and is not only computing <strong>the</strong><br />

servo error, but is also mentally modelling <strong>the</strong> machine’s response to avoid instability.<br />

<strong>The</strong> pilot may also be providing all <strong>of</strong> <strong>the</strong> control power with his own muscles. This<br />

task must be performed for <strong>the</strong> duration <strong>of</strong> <strong>the</strong> flight, as <strong>the</strong> machine will diverge if<br />

attention lapses for more than a few seconds.

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