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- 宮本 侑斗
- 九州大学大学院工学府航空宇宙工学専攻
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- 原田 明徳
- 九州大学大学院工学府航空宇宙工学専攻
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- ビクラマシンハ ナヴィンダ キトマル
- 九州大学大学院工学府航空宇宙工学専攻
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- 宮沢 与和
- 九州大学大学院工学研究院航空宇宙工学部門
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- 船曳 孝三
- 日本航空株式会社
書誌事項
- タイトル別名
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- Evaluation Analysis on Airliner Operational Performance with Flight Trajectory Optimization using BADA Aircraft Performance Model
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説明
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.
収録刊行物
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- 航空宇宙技術
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航空宇宙技術 13 (0), 1-10, 2014
一般社団法人 日本航空宇宙学会
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詳細情報 詳細情報について
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- CRID
- 1390282680296475648
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- NII論文ID
- 130003395501
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- ISSN
- 18840477
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- 本文言語コード
- ja
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- データソース種別
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- JaLC
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可