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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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Fig. 7.49 In <strong>the</strong> Lockheed AMCS, <strong>the</strong> gyro is caused to precess by springs as before, but <strong>the</strong> gyro motion<br />

controls actuators that drive <strong>the</strong> swashplate. This prevents control forces disturbing <strong>the</strong> gyro.<br />

<strong>the</strong> same level <strong>of</strong> training as his full-size counterpart. Beginners <strong>of</strong>ten fit extra weights to<br />

<strong>the</strong> flybar to reduce <strong>the</strong> following rate even fur<strong>the</strong>r. <strong>The</strong> flybar also allows <strong>the</strong> use <strong>of</strong> inexpensive<br />

and lightweight wooden blades whose following rate alone would be too fast.<br />

<strong>The</strong> Bell system was difficult to replicate in miniature because <strong>of</strong> <strong>the</strong> hydraulic<br />

dampers, and <strong>the</strong> pure Hiller system was found to produce a very low following rate<br />

in models. As a result a hybrid system combining both and aptly called <strong>the</strong> Bell-Hiller<br />

system evolved. This uses <strong>the</strong> cyclic mixing <strong>of</strong> <strong>the</strong> Bell bar, as well as <strong>the</strong> Hiller paddles<br />

and control rotor fea<strong>the</strong>ring. <strong>The</strong>re are thus three rods coming from <strong>the</strong> swashplate: one<br />

to each <strong>of</strong> <strong>the</strong> flybar mixer arms, and one to fea<strong>the</strong>r <strong>the</strong> control rotor. This arrangement<br />

gives a good balance between stability and response, although <strong>the</strong> number <strong>of</strong><br />

links involved makes it look like a dog’s dinner. <strong>The</strong> falling cost <strong>of</strong> <strong>the</strong> piezo-electric<br />

gyroscope and its minute size mean that <strong>the</strong> flybar can now be eliminated in <strong>the</strong> model<br />

helicopter.<br />

7.27 Autopilots and AFCS<br />

Autopilots vary in complexity, but <strong>the</strong> general goal is that <strong>the</strong> pilot is relieved <strong>of</strong> <strong>the</strong><br />

need to maintain some parameter <strong>of</strong> <strong>the</strong> flight. In a helicopter it is possible to begin<br />

with stabilization <strong>of</strong> <strong>the</strong> roll axis only, and <strong>the</strong>n add extra features. Automatic control<br />

<strong>of</strong> <strong>the</strong> tail rotor allows balanced turns and flight at minimum drag. Control <strong>of</strong> <strong>the</strong> pitch<br />

axis allows <strong>the</strong> airspeed to be held, and altitude can be held with collective control.<br />

Some systems can achieve a stable hover in a fixed location without pilot intervention.<br />

Control 313

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