Mathematical modelling of aircraft electrical power systems

2013-12-17T15:15:51Z (GMT) 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.