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Please use this identifier to cite or link to this item: https://dspace.lboro.ac.uk/2134/13859

Title: Mathematical modelling of aircraft electrical power systems
Authors: Vadher, Vinod V.
Issue Date: 1981
Publisher: © Vinod Vashram Vadher
Abstract: 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.
Description: A Doctoral Thesis. Submitted in partial fulfilment of the requirements for the award of Doctor of Philosophy of Loughborough University.
URI: https://dspace.lboro.ac.uk/2134/13859
Appears in Collections:PhD Theses (Mechanical, Electrical and Manufacturing Engineering)

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