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Mathematical modelling of aircraft electrical power systems
thesis
posted on 2013-12-17, 15:15 authored by Vinod V. VadherThe 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 VadherPublication date
1981Notes
A Doctoral Thesis. Submitted in partial fulfilment of the requirements for the award of Doctor of Philosophy of Loughborough University.Language
- en
