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Optimization and sensitivity studies of flight-path trajectoriesThe optimization of landing trajectories of the Boeing 737 is presented. The primary factor considered was the noise delivered to the population residing near an air terminal but passenger comfort, fuel consumption and time elapsed during the maneuver were also considered. A digital simulation of the aircraft, a noise model and a passenger comfort model, was completed. The digital simulation was made more efficient time-wise. A population model for an urban area was developed and the noise model was integrated into the population model. A steepest descent optimization algorithm was programmed. Some constant glide slope trajectories into an urban Airport were simulated and evaluated with respect to the performance index, and their ground track plotted.
Document ID
19750024048
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Cook, G.
(Virginia Univ. Charlottesville, VA, United States)
Witt, R. M.
(Virginia Univ. Charlottesville, VA, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1975
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
EE-4038-102-75
NASA-CR-119132
Report Number: EE-4038-102-75
Report Number: NASA-CR-119132
Accession Number
75N32121
Funding Number(s)
CONTRACT_GRANT: NSG-1101
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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