The paper attempts to delineate the multi-technology, multi-variate nature of the flight vehicle and the complex interactions between the various areas involved in its synthesis. Considerations arising in the choice and configuration layout of the hardware for tactical aircraft are outlined. A brief mathematical formulation of a system oriented approach to design is proposed for optimizing the flight vehicle parameters.
Multi-Variate Optimization Problems of Flight Vehicle Synthesis
1978
42 pages
Report
Keine Angabe
Englisch
NTRS | 1971
|British Library Conference Proceedings | 2010
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