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Military Communications and Information Technology: A Trusted ...

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Modern Low Cost Aircraft Instruments<br />

Radek Bystricky 1 , Premysl Janu 2<br />

1 Department of Aerospace Electrical Systems<br />

2 Department of Radar <strong>Technology</strong>, Faculty of <strong>Military</strong> <strong>Technology</strong>,<br />

University of Defence, Brno, Czech Republic,<br />

{radek.bystricky, premysl.janu}@unob.cz<br />

Abstract: The usage of multifunction displays (MFD) in nowadays aircraft boards is about to increase.<br />

They are usually able to show a big number of relevant information at once, so their contribution<br />

cannot be denied. But it is hard to imagine that, in case of emergency (e.g., space disorientation),<br />

the pilot will browse between pages on the display. In this case, he immediately needs to know basic<br />

information about speed, altitude, etc. <strong>and</strong> will therefore rather rely on conventional gauges instruments.<br />

This paper therefore deals with the design <strong>and</strong> development of classical <strong>and</strong> especially cheap<br />

gauge instrument connected the on-board data bus.<br />

Keywords: MFD; aircraft instrument; CAN; CANaerospace; microcontroler, Time-triggered<br />

I. Introduction<br />

First we need to ask ourselves what must be an inexpensive aircraft instrument<br />

able to do, except that it must be accurate, reliable <strong>and</strong> rugged. It must be able to<br />

measure the flight parameter with sufficient accuracy at first. It is also advantageous<br />

if this flight parameter can be transmitted to other devices using some kind<br />

of a data bus. Finally, it must have sufficiently precise scale with a fine gauge step<br />

<strong>and</strong> be able to detect their own faults <strong>and</strong> report them.<br />

II. Hardware conception<br />

Our concept is based on the division of the device into individual components<br />

that can exist independent to the measured flight parameter. This concept is adopted<br />

from real instruments build by Czech company MESIT <strong>and</strong> used for example on<br />

the aircraft L159 ALCA, see Figure 1. But the concept itself is the only thing what<br />

ours instruments replicates [1]. The rest differs significantly.<br />

Basic components are:<br />

• Power block.<br />

• Signal processing block.

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