• ISSN 0258-2724
  • CN 51-1277/U
  • EI Compendex
  • Scopus
  • Indexed by Core Journals of China, Chinese S&T Journal Citation Reports
  • Chinese S&T Journal Citation Reports
  • Chinese Science Citation Database
Volume 54 Issue 1
Feb.  2019
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Article Contents
DAI Fuqing, PANG Bizhao, ZHAO Yuandi. Air Route Crossing Angles Optimization Model with Different Preferences[J]. Journal of Southwest Jiaotong University, 2019, 54(1): 180-188. doi: 10.3969/j.issn.0258-2724.20170798
Citation: DAI Fuqing, PANG Bizhao, ZHAO Yuandi. Air Route Crossing Angles Optimization Model with Different Preferences[J]. Journal of Southwest Jiaotong University, 2019, 54(1): 180-188. doi: 10.3969/j.issn.0258-2724.20170798

Air Route Crossing Angles Optimization Model with Different Preferences

doi: 10.3969/j.issn.0258-2724.20170798
  • Received Date: 09 Nov 2017
  • Rev Recd Date: 10 May 2018
  • Available Online: 08 Jul 2018
  • Publish Date: 01 Feb 2019
  • In order to investigate the internal mechanism of influence on air traffic posed by airspace structure and to clear bottlenecks of air traffic operation at air transit network nodes, the optimization of air route crossing angles was studied. After analysing the relationship between flight time, fuel consumption, and the angles of basic intersection route structure, an integrated crossing route angle structure was set up. Then, based on the air traffic flow distribution trait of the crossing routes, a preference mathematical model was developed to optimize the crossing angles in terms of flight time and fuel consumption. Finally, a representative crossing route was selected to verify the proposed model. The results show a negative linear correlation between flight time and fuel consumption and a 0.54% increase in total flight costs if flight time is solely considered versus a 2.89% decrease if only fuel consumption is taken into account. There is, however, a 3.82% reduction in total flight costs without preferences or 5.26% (the minimum value of total flight costs obtained when flight time coefficient equals 0.4) with preferences. The average amounts of fuel consumption density, flight conflicts, and controller workloads also declined 20.41%, 56.12%, and 46.24%, respectively, but the original airspace angle structure changed a mere 11.88% after the optimization.

     

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