日本航空宇宙学会論文集
Online ISSN : 2432-3691
Print ISSN : 1344-6460
ISSN-L : 1344-6460
論文
フルフライトシミュレータによる降下角を固定した継続降下運航の評価
伊藤 恵理福島 幸子平林 博子ビクラマシンハ ナヴィンダ キトマル
著者情報
ジャーナル フリー

2016 年 64 巻 1 号 p. 50-57

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抄録
In an effort to realize efficient arrival operations, one of the challenges directs at realizing energy-saving arrivals is Continuous Descent Operation (CDO), with which the arrival aircraft descends to the airport continuously using near-idling thrust. As a potential solution to achieve both time-spacing performance and fuel reduction while conducting CDO in arrival traffic, this paper suggests applying ``Fixed-flight Path Angle (FPA) descent,'' which the arrival aircraft continuously descents to the assigned runway following the fixed vertical path angles. The feasibility of the FPA descent was evaluated via a series of B777-200 full-flight simulator experiments, eleven trials in total. With the use of airline's flight simulator, the pilot's operability and tracking performance following the assigned FPA vertical path were assessed. The effectiveness of the combination of FPA descent and speed control is clarified via a comparison with conventional arrival operations. These simulation results show the applicability of the proposed FPA descent and suggest its future contributions.
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© 2016 The Japan Society for Aeronautical and Space Sciences
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