Since inverter induced instability is system problem, analysis of whole aircraft d-c power system is presented to point out measurable properties which may be used to predict stability. (See also Am Inst Elec Engrs -- Trans v 76 (Applications and Industry) n 32 Sept 1957 p 183-8)
Stability of aircraft D-C power systems with inverter loads
Elec Eng
Electrical Engineering ; 76 , n 10
1957
Article (Journal)
English
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Aircraft Electrical Power Systems and Nonlinear Dynamic Loads
SAE Technical Papers | 2012
|NTIS | 2001
|Wiley | 2014
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