Volume 49 Issue 1
Jan.  2023
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ZHANG J F,YOU L B,ZHOU M,et al. Multi-objective arrival sequencing and scheduling based on point merge system[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(1):66-73 (in Chinese) doi: 10.13700/j.bh.1001-5965.2021.0199
Citation: ZHANG J F,YOU L B,ZHOU M,et al. Multi-objective arrival sequencing and scheduling based on point merge system[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(1):66-73 (in Chinese) doi: 10.13700/j.bh.1001-5965.2021.0199

Multi-objective arrival sequencing and scheduling based on point merge system

doi: 10.13700/j.bh.1001-5965.2021.0199
Funds:  National Natural Science Foundation of China (U1933117)
More Information
  • Corresponding author: E-mail:zhangjunfeng@nuaa.edu.cn
  • Received Date: 19 Apr 2021
  • Accepted Date: 04 Jul 2021
  • Available Online: 16 Jan 2023
  • Publish Date: 26 Jul 2021
  • Increasing traffic demand and the saturated terminal airspace call for safer flight performance and more efficient control performance. Therefore, this paper focuses on the multi-objective arrival sequencing and scheduling based on point merge system (PMS). Firstly, the four-dimensional trajectory prediction model was developed to predict future trajectories since trajectory prediction played a critical role in arrival sequencing and scheduling. Secondly, the PMS-based multi-objective arrival sequencing model was put forward while taking both the PMS operation modes and different stakeholders appeals into account. Moreover, the multi-objective imperialist competition algorithm (ICA) was proposed based on a non-dominated sorting strategy for solving such a problem. Finally, the data from the Monte Carlo simulation and actual operating of Changsha Huanghua International Airport were used for validation. The results indicated that the proposed method was effective and efficient. On the one hand, the proposed multi-objective ICA did well in practical application, making decision support for controllers. On the other hand, the proposed method could reduce the total delay time, total flight time, and maximum flight time by 70.8%, 13.2%, and 11.8%, compared with the actual operation, with relatively conservative safety separations.

     

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