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Mathematical modelling of aircraft electrical power systems

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thesis
posted on 17.12.2013 by Vinod V. Vadher
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.

History

School

  • Mechanical, Electrical and Manufacturing Engineering

Publisher

© Vinod Vashram Vadher

Publication date

1981

Notes

A Doctoral Thesis. Submitted in partial fulfilment of the requirements for the award of Doctor of Philosophy of Loughborough University.

Language

en

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