The continuing developments in aircraft electrical power
supply systems have been accompanied by a progressive narrowing
of the transient and the steagy-state voltage regulation limits
within which the system must operate. The performance of a system
is satisfactory only when it meets the conditions of the relevant
performance specification, for example MIL-G-2l480A (AS), as laid
down by the aircraft manufacturer...cont'd.
A Doctoral Thesis. Submitted in partial fulfilment of the requirements for the award of Doctor of Philosophy of Loughborough University.