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Evaluation Analysis on Airliner Operational Performance with Flight Trajectory Optimization using BADA Aircraft Performance Model
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- MIYAMOTO Yuto
- 九州大学大学院工学府航空宇宙工学専攻
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- HARADA Akinori
- 九州大学大学院工学府航空宇宙工学専攻
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- WICKRAMASINGHE Navinda Kithmal
- 九州大学大学院工学府航空宇宙工学専攻
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- MIYAZAWA Yoshikazu
- 九州大学大学院工学研究院航空宇宙工学部門
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- FUNABIKI Kozo
- 日本航空株式会社
Bibliographic Information
- Other Title
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- BADAモデルを用いた旅客機の軌道最適化による運航効率の評価
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Description
Fuel efficient flight is demanded due to air traffic increase, environmental concerns and skyrocketing fuel prices. To achieve an effective futuristic air traffic management system, realization of TBO (Trajectory Based Operations) optimized from departure to arrival is aimed in CARATS (Collaborative Actions for Renovation of Air Traffic Systems). In this paper, 4-D trajectory of passenger aircraft is optimized for fuel minimization on the assumption that aircraft is not bounded by any air traffic control constraints. BADA (Base of Aircraft Data) model is adopted for aircraft performance model, and dynamic programming is used to calculate the optimal trajectory. The optimal trajectory is compared with airliner’s flight trajectory by evaluating fuel consumption, flight time and flight range. Examples show that considerable amounts of reduction in fuel consumption could be achieved by trajectory optimization compared to the estimated values of actual flights.
Journal
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- AEROSPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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AEROSPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 13 (0), 1-10, 2014
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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Details 詳細情報について
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- CRID
- 1390282680296475648
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- NII Article ID
- 130003395501
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- ISSN
- 18840477
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- Text Lang
- ja
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- Data Source
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- JaLC
- Crossref
- CiNii Articles
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- Abstract License Flag
- Disallowed