JP6034130B2 - 航空機パラメータを推定するための方法およびシステム - Google Patents
航空機パラメータを推定するための方法およびシステム Download PDFInfo
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- JP6034130B2 JP6034130B2 JP2012233352A JP2012233352A JP6034130B2 JP 6034130 B2 JP6034130 B2 JP 6034130B2 JP 2012233352 A JP2012233352 A JP 2012233352A JP 2012233352 A JP2012233352 A JP 2012233352A JP 6034130 B2 JP6034130 B2 JP 6034130B2
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- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/0095—Aspects of air-traffic control not provided for in the other subgroups of this main group
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Description
Claims (7)
- 航空機の軌道を予測するために軌道予測器が使用することができる航空機性能パラメータを推定する方法であって、
航空交通制御システムにより、予測垂直プロファイルの少なくとも1つの変更点を含む、航空機に関する軌道予測情報を受け取るステップと、次に
前記航空交通制御システムで実施されるパラメータ推定プロセスで、さもなければ地上自動化システムには未知である前記航空機の航空機性能パラメータを推定するために前記軌道予測情報を使用するステップと、
を含み、
前記パラメータ推定プロセスは、航空機性能パラメータの所定の値に割り当てられたより高い確率で初期化される確率密度関数および前記航空機の前記航空機性能パラメータを予測し且つ改良するための更新プロセスを利用し、
前記軌道予測情報が、前記航空機の少なくとも1つの軌道変更点の相対位置を含み、
前記航空機性能パラメータが、前記少なくとも1つの軌道変更点の前記相対位置から推定される前記航空機の離陸重量を含み、
前記少なくとも1つの軌道変更が、上昇飛行の頂点または降下の頂点のうちの少なくとも1つを含む、
方法。 - 前記航空機に関する前記軌道予測情報が前記航空機から伝送される、請求項1に記載の方法。
- 前記受け取るステップが、前記航空機と前記地上自動化システムの間の通信リンクの使用を含む、請求項2に記載の方法。
- 前記方法が、前記航空機の軌道を予測するために、前記航空機性能パラメータを前記地上自動化システムの1つまたは複数の軌道予測器に適用するステップをさらに含む、請求項1に記載の方法。
- 前記使用するステップが、前記航空機の前記軌道予測情報を、軌道予測器を使用して、前記航空機の前記航空機性能パラメータを可能な値全体にわたって変化させることによって生成された一組の航空機性能情報と比較するステップと、次に前記比較に基づいて少なくとも1つの航空機性能パラメータを更新するステップによって前記航空機の前記航空機性能パラメータのうちの前記少なくとも1つを予測するステップを含む、請求項1に記載の方法。
- 前記使用するステップが、前記航空機の前記航空機性能パラメータを推定するために前記航空機の監視および測定データを使用するステップをさらに含む、請求項1に記載の方法。
- 前記航空機性能パラメータのそれぞれを確率密度関数によって表すことによって、前記航空機性能パラメータを初期化するステップをさらに含む、請求項1に記載の方法。
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/285,259 US8798898B2 (en) | 2011-10-31 | 2011-10-31 | Methods and systems for inferring aircraft parameters |
US13/285,259 | 2011-10-31 |
Publications (3)
Publication Number | Publication Date |
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JP2013096988A JP2013096988A (ja) | 2013-05-20 |
JP2013096988A5 JP2013096988A5 (ja) | 2015-12-03 |
JP6034130B2 true JP6034130B2 (ja) | 2016-11-30 |
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JP2012233352A Expired - Fee Related JP6034130B2 (ja) | 2011-10-31 | 2012-10-23 | 航空機パラメータを推定するための方法およびシステム |
Country Status (5)
Country | Link |
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US (1) | US8798898B2 (ja) |
EP (1) | EP2587464B1 (ja) |
JP (1) | JP6034130B2 (ja) |
CN (1) | CN103093649B (ja) |
CA (1) | CA2793457C (ja) |
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CN112882488B (zh) * | 2021-01-11 | 2022-08-05 | 成都民航空管科技发展有限公司 | 航空器4d轨迹预测方法及装置 |
CN112927562B (zh) * | 2021-01-28 | 2022-03-04 | 中国电子科技集团公司第二十八研究所 | 一种基于指定高度限制的航空器飞行高度剖面计算方法 |
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2011
- 2011-10-31 US US13/285,259 patent/US8798898B2/en active Active
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2012
- 2012-10-23 JP JP2012233352A patent/JP6034130B2/ja not_active Expired - Fee Related
- 2012-10-25 CA CA2793457A patent/CA2793457C/en active Active
- 2012-10-30 EP EP12190580.6A patent/EP2587464B1/en active Active
- 2012-10-31 CN CN201210426479.6A patent/CN103093649B/zh active Active
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Publication number | Publication date |
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CN103093649A (zh) | 2013-05-08 |
CA2793457C (en) | 2019-11-19 |
EP2587464B1 (en) | 2018-09-26 |
CN103093649B (zh) | 2018-09-07 |
US20130110387A1 (en) | 2013-05-02 |
US8798898B2 (en) | 2014-08-05 |
EP2587464A1 (en) | 2013-05-01 |
CA2793457A1 (en) | 2013-04-30 |
JP2013096988A (ja) | 2013-05-20 |
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