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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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O<strong>the</strong>r types <strong>of</strong> rotorcraft 377<br />

Fig. 9.29 UAV with coaxial rotors and a rotationally symmetrical body can attain high speeds by near-axial<br />

flight.<br />

be used for tasks in which <strong>the</strong>re is a significant risk. Pilotless aircraft are <strong>of</strong>ten called<br />

drones and <strong>the</strong> term is also applied to pilotless helicopters.<br />

Small remotely controlled helicopters can be used for reconnaissance and may escape<br />

detection or prove very difficult targets if <strong>the</strong>y are detected. Small helicopters have<br />

also been developed for crop dusting, notably in Japan. However, <strong>the</strong> limitations <strong>of</strong><br />

<strong>the</strong> helicopter apply to small ones equally. Small fixed-wing drones can be launched<br />

from a simple ramp and recovered by parachute and will have greater range than<br />

<strong>the</strong> inefficient helicopter. Consequently drone helicopters are very rare indeed and fill<br />

extremely specialized niches.<br />

<strong>The</strong> drone helicopter may depend entirely on a remote pilot, or it may be entirely<br />

autonomous so that it can complete an entire mission automatically. Early drones were<br />

totally pilot controlled and had to stay within sight <strong>of</strong> <strong>the</strong> pilot. Subsequently <strong>the</strong> drone<br />

could relay a television picture <strong>of</strong> <strong>the</strong> view from <strong>the</strong> cockpit so that <strong>the</strong> drone could<br />

be flown out <strong>of</strong> sight. As electronics developed, it became possible to integrate <strong>the</strong><br />

helicopter controls with autopilot functions and control <strong>the</strong> whole with a navigation<br />

system. This led to <strong>the</strong> UAV (unmanned air vehicle) concept that can be applied to <strong>the</strong><br />

helicopter as well as it can to <strong>the</strong> aeroplane.<br />

In <strong>the</strong> absence <strong>of</strong> a pilot <strong>the</strong> UAV designer has much more freedom. <strong>The</strong> contrarotating<br />

coaxial rotor is popular as it avoids <strong>the</strong> use <strong>of</strong> very small and delicate tail<br />

rotors. Figure 9.29 shows a typical UAV having coaxial rotors. <strong>The</strong> hull is axially<br />

symmetrical and high speed forward flight can be achieved by tilting <strong>the</strong> whole machine<br />

over. Tilt-rotor UAVs have also been developed.<br />

9.11 Radio control principles<br />

Radio control is simply <strong>the</strong> use <strong>of</strong> radio signals to relay <strong>the</strong> position <strong>of</strong> control sticks<br />

without any physical connection. In practical applications <strong>the</strong>re will be a need to have<br />

several control channels simultaneously available and each one will need to be proportional,<br />

which means that small or large movements <strong>of</strong> <strong>the</strong> control stick will be remotely<br />

reproduced by <strong>the</strong> movement <strong>of</strong> a servo.<br />

<strong>The</strong> foundation <strong>of</strong> this technology was a patent by A.H. Reeves in <strong>the</strong> 1930s which<br />

showed that any type <strong>of</strong> information could be carried by varying <strong>the</strong> width or distribution<br />

<strong>of</strong> pulses. In a helicopter, <strong>the</strong> actual flying controls require four simultaneous

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