König, Reinhard and Schubert, E. (2011) On the Influences of an Increased ILS Glide Slope on Noise Impact, Fuel Consumption and Landing Approach Operation. AIAC14 Fourteenth Australian International Aerospace Congress, 28. Feb. - 3. March 2011, Melbourne, Australia.
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This paper will show the theoretical influences of an increased glide slope to noise impact and fuel consumption. It will describe the risk of procedure changes made by the pilots to cope with a steeper descent. Furhermore, the development of a simulator study, the achieved results with regard to safety and operational aspects and the outcome of performance simulations for different aircraft types will be described. As a result glide slopes up to 3.2° could be realized without the necessity of flight procedural changes from performance and pilots view. Based on this fact the Frankfurt/Main Airport will conduct a test operation of a 3.2° ILS for noise purposes on the new north-west landing runway, which constructions is in progress.
|Document Type:||Conference or Workshop Item (Speech)|
|Title:||On the Influences of an Increased ILS Glide Slope on Noise Impact, Fuel Consumption and Landing Approach Operation|
|In ISI Web of Science:||No|
|Keywords:||Steep Approach, Noise Impact, Noise Abatement, Fuel Consumption, Landing Operation|
|Event Title:||AIAC14 Fourteenth Australian International Aerospace Congress|
|Event Location:||Melbourne, Australia|
|Event Type:||international Conference|
|Event Dates:||28. Feb. - 3. March 2011|
|HGF - Research field:||Aeronautics, Space and Transport|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||other|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L - no assignement|
|DLR - Research theme (Project):||L -- no assignement|
|Institutes and Institutions:||Institute of Flight Systems > Flight Dynamics and Simulation|
|Deposited By:||Tanja Bracke|
|Deposited On:||29 Mar 2011 14:02|
|Last Modified:||18 Jan 2012 11:09|
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