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The Development of Neural Network Based System Identification ...

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70 CHAPTER 3 AERIAL PLATFORM AND CUSTOM-BUILT FLIGHT TEST SYSTEM<br />

where L 1 and L 2 indicate the length <strong>of</strong> arm 1 and 2 respectively.<br />

Due to cost constraints, it was decided that positional measurements should be<br />

accurate to 1%. To achieve this accuracy in the XY plane, the encoders must have a<br />

resolution finer than 0.57 ◦ (θ = sin −1 (1%)). <strong>The</strong> Romuron A6A2-CWZ3E incremental<br />

optical encoder was selected for this project, with sufficient accuracy (θ = 360 ◦ /2000 =<br />

0.18 ◦ revolution) for a prototype. <strong>The</strong> encoder is compact and has a very small starting<br />

torque, so it will easily fit into confined spaces and will not add any dynamic effects to<br />

the test stand.<br />

In order to measure the altitude <strong>of</strong> the helicopter, a linear position transducer<br />

is used to monitor the actual altitude reading <strong>of</strong> the helicopter. <strong>The</strong> linear position<br />

transducer is mounted at the side <strong>of</strong> the sliding vertical mechanism as shown in the<br />

Figure 3.11.<br />

<strong>The</strong> UniMeasure LX-PA-30 linear position transducer was chosen to<br />

measure the displacement <strong>of</strong> the sliding vertical arm. <strong>The</strong> unit consists <strong>of</strong> a precision<br />

potentiometer, attached to a spring loaded string (maximum extension = 750 mm),<br />

which unwinds as the vertical arm is extended. It has linearity <strong>of</strong> ±0.25% which produce<br />

distance measurement accuracy up to 1.875 mm. <strong>The</strong>re are also dead band regions at<br />

the maximum and minimum allowable displacements which need to be accounted for in<br />

the string length displacement, l calculation. <strong>The</strong> linear transducer outputs an analog<br />

signal measurement and this signal is converted to digital signal with 12-Bit MCP3221<br />

A/D converter chip with I 2 C interface. <strong>The</strong> signal received from the A/D converter<br />

chip is used to calculate the length <strong>of</strong> the string, l by the following relationship:<br />

V in = V dd × A in<br />

l (mm) =<br />

2 12<br />

V in − V o,low<br />

V dd − V o,low − V o,high<br />

× 750 (3.3)<br />

where A in and V dd denote output voltage and excitation voltage supplied to the potentiometer.<br />

V o,low and V o,high indicate the <strong>of</strong>fset voltages <strong>of</strong> the potentiometer corresponding<br />

to the lowest (initial) and highest (maximum) string displacement. Since the<br />

linear transducer is not placed parallel with the vertical arm, a simple modification is<br />

further made into the altitude measurement from the linear transducer. Figure 3.12

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