Although all sensors will have differing requirements the principles described in this paper can be applied to every integration task. To demonstrate the technique it assumed that a requirement exists to assist the crew in poor visibility by fitting a low light sensor. The requirement, and aircraft system to which it is to be fitted are fictitious, although they are representative of current systems. The method used is Top Down Design which takes the original requirement, breaks it down to its various Functions and Processes and then recreates it into various Line Replaceable Units, and Software Requirements, in a structured computer compatible format.
Integration of a new sensor on to an existing aircraft
Die Integration eines neuen Messwertaufnehmers in ein bestehendes Flugzeug
1983
7 Seiten, 1 Tabelle
Report
Englisch
Weapon Systems Integration in Existing Aircraft
British Library Conference Proceedings | 1999
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