A control system of permanent magnet synchronous motor ensuring its fail-safety at the expense of switchover between several scalar control modes, is proposed. A computer simulation model is realized. The operation of such a system is analyzed in terms of the electric pump unit of space application.
Fail-Safe Control System for an Electric Pump Unit of Space Application
Russ. Aeronaut.
Russian Aeronautics ; 64 , 2 ; 210-218
2021-04-01
9 pages
Article (Journal)
Electronic Resource
English
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