The way to optimize a flight program of subsonic passenger aircraft at lowering and braking of the aircraft by considering operational constraints for civil aviation
Published: 27.10.2015
Authors: Gubareva E.A., Mozzhorina T.Yu.
Published in issue: #8(44)/2015
DOI: 10.18698/2308-6033-2015-8-1415
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control
Flight simulation is based on traditional approaches used for subsonic passenger aircrafts. Lowering and braking modes of operation are optimized by considering operational constraints for civil aviation. For simulating flight conditions we used the in-built model of bypass turbojet engine. It makes possible to calculate power plant parameters under any flight conditions.
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