Optimization of rotorcraft flight following engine failure
Optimization of rotorcraft flight following engine failure
- New search for: Jhemi, Ali A.
- New search for: Carlson, Erich B.
- New search for: Zhao, Yiyuan J.
- New search for: Chen, Robert T.N.
- New search for: Jhemi, Ali A.
- New search for: Carlson, Erich B.
- New search for: Zhao, Yiyuan J.
- New search for: Chen, Robert T.N.
Dynamic optimization methods can be used to provide quick and low-cost iterations in rotorcraft analysis and design, and to generate benchmark results for flight tests. In this paper, key steps in the effective application of dynamic optimization methods are identified. Numerical solution algorithms are reviewed. The uses ofdynamic optimization methods are illustrated with examples offlight path optimizations for both helicopter and tiltrotor aircraft following engine failure. In these examples, flights after an engine failure are formulated as dynamic optimization problems. Performance indices and constraints are properly selected so that conclusions can be drawn about rotorcraft performance boundaries following an engine failure.
Document information
Optimization of rotorcraft flight following engine failure
Optimierung des Hubschrauberfluges nach Antriebsausfall
Journal of the American Helicopter Society ; 49 , 2 ; 117-126
2004
10 Seiten, 9 Bilder, 1 Tabelle, 27 Quellen
Article (Journal)
English
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