Mathematical modelling of aircraft electrical power systems
thesisposted on 17.12.2013, 15:15 authored 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.
- Mechanical, Electrical and Manufacturing Engineering