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oaioai:casi.ntrs.nasa.gov:19770011193

Simulator evaluation of optimal thrust management/fuel conservation strategies for airbus aircraft on short haul routes

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1977
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Abstract

The feasibility of incorporating optimal concepts into a practical system was determined. Various earlier theoretical analyses were confirmed, and insight was gained into the sensitivity of fuel conservation strategies to nonlinear and second order aerodynamic and engine characteristics. In addition to the investigation of optimal trajectories the study ascertained combined fuel savings by utilizing various procedure-oriented improvements such as delayed flap/decelerating approaches and great circle navigation

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This paper was published in NASA Technical Reports Server.

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