发明名称 飛行経路導出装置および飛行経路導出方法
摘要 PROBLEM TO BE SOLVED: To stably suppress noise received by each point on the ground to an assumed level or less regardless of changes of noise distribution due to a weather condition.SOLUTION: A flight path deriving apparatus 120 is equipped with: a noise distribution acquisition section 150 which acquires noise distribution that occurs when an aircraft flew on a standard flight path being a standard flight path; a deviation amount transition deriving section 170 which derives deviation amount transition showing transition of a deviation amount of noise with respect to the standard flight path based on the noise distribution; a symmetric transition deriving section 172 which derives symmetric transition symmetrical to the deviation amount transition by using the standard flight path as a reference; and a revised flight path deriving section 174 which derives a revised flight path on which an aircraft can fly based on the symmetric transition.
申请公布号 JP6047741(B2) 申请公布日期 2016.12.21
申请号 JP20120166458 申请日期 2012.07.27
申请人 富士重工業株式会社;国立研究開発法人宇宙航空研究開発機構 发明人 岡田 悟史;石井 寛一;奥野 善則
分类号 B64D45/00 主分类号 B64D45/00
代理机构 代理人
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