New Aircraft Avionics installation and functionality

New Aircraft Avionics installation and functionality

produce a report on installing a hypothetical avionics systems on an aircraft which lacks any type of avionics systems. This should be written from the standpoint that you have been tasked as a design engineer to develop a full avionics package for a new aircraft. Using this aircraft as a ‘blank canvas’ you are to describe the functionality of 5 different systems while detailing in depth at least 2 of these. This report should be properly introduced and concluded and cover the following topics:

* The Basic theory and function of 3 out of a chosen 5 hypothetical avionics systems.

* Describe and show a block diagram, electrical cable routing and power source wiring for the above 3 systems.

* Detail the operation of the remaining 2 out of the 5 hypothetical avionics systems. This should include:

o Describe and show a block diagram, electrical cable routing and power source wiring.

o An in depth description of the systems themselves that should include the exact functions of each system.

o The details of any peripherals.

o State which system(s) should employ some form of redundancy, how this is employed and why.
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Referencing Requirements:
correct Harvard referencing is a must, using authoritative sources, using easy English language
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