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Design of an integrated airframe/propulsion control system architecture
- Publication Year :
- 1990
- Publisher :
- United States: NASA Center for Aerospace Information (CASI), 1990.
-
Abstract
- The design of an integrated airframe/propulsion control system architecture is described. The design is based on a prevalidation methodology that used both reliability and performance tools. An account is given of the motivation for the final design and problems associated with both reliability and performance modeling. The appendices contain a listing of the code for both the reliability and performance model used in the design.
- Subjects :
- Systems Analysis
Subjects
Details
- Language :
- English
- Database :
- NASA Technical Reports
- Notes :
- NAS1-18099, , RTOP 505-66-71-02
- Publication Type :
- Report
- Accession number :
- edsnas.19920013400
- Document Type :
- Report