Task 1:

Carry out a detailed comparison between mechanical, fluid and electrical methods of power generation for a typical aircraft usage.

Task 2:

Design an aircraft power distribution system and explain the features of your system that help to ensure the continuing integrity and safety.

Task 3:

Scenario:

As a qualified aircraft control systems designer, you have been tasked with choosing an appropriate servo/actuation system that will enable the smooth operation of proposed new large passenger aircraft's control surfaces. Your choice will be presented to the aircraft manufacturer.

Your presentation should include details of the following:

Construction,

Control,

Protection methods,

Performance parameters of electric motors and actuators used