Design of a microprocessor-based Control, Interface and Monitoring (CIM unit for turbine engine controls research
United States: NASA Center for Aerospace Information (CASI), 1983
Online
report
High speed minicomputers were used in the past to implement advanced digital control algorithms for turbine engines. These minicomputers are typically large and expensive. It is desirable for a number of reasons to use microprocessor-based systems for future controls research. They are relatively compact, inexpensive, and are representative of the hardware that would be used for actual engine-mounted controls. The Control, Interface, and Monitoring Unit (CIM) contains a microprocessor-based controls computer, necessary interface hardware and a system to monitor while it is running an engine. It is presently being used to evaluate an advanced turbofan engine control algorithm.
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Design of a microprocessor-based Control, Interface and Monitoring (CIM unit for turbine engine controls research
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Autor/in / Beteiligte Person: | Delaat, J. C ; Soeder, J. F |
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Veröffentlichung: | United States: NASA Center for Aerospace Information (CASI), 1983 |
Medientyp: | report |
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