WEKO3
アイテム
Development of Control Advisory System Using Future Wind Information
http://hdl.handle.net/2261/00074960
http://hdl.handle.net/2261/0007496093ef8f2f-00b2-444f-a526-3452bfa7d15c
名前 / ファイル | ライセンス | アクション |
---|---|---|
![]() |
|
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2018-08-22 | |||||
タイトル | ||||||
タイトル | Development of Control Advisory System Using Future Wind Information | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Control Advice | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Cockpit Display | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Human Pilot | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Doppler LIDAR | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Energy Principle | |||||
資源タイプ | ||||||
資源 | http://purl.org/coar/resource_type/c_5794 | |||||
タイプ | conference paper | |||||
著者 |
Kamo, Shumpei
× Kamo, Shumpei× Entzinger, Jorg Onno× Uemura, Tsuneharu× Suzuki, Shinji |
|||||
著者別名 | ||||||
識別子Scheme | WEKO | |||||
識別子 | 147954 | |||||
姓名 | 加茂, 舜平 | |||||
著者別名 | ||||||
識別子Scheme | WEKO | |||||
識別子 | 147955 | |||||
姓名 | エントジンガー, ヨルグ オノ | |||||
著者別名 | ||||||
識別子Scheme | WEKO | |||||
識別子 | 147956 | |||||
姓名 | 上村, 常治 | |||||
著者別名 | ||||||
識別子Scheme | WEKO | |||||
識別子 | 147957 | |||||
姓名 | 鈴木, 真二 | |||||
著者所属 | ||||||
著者所属 | Department of Aeronautics and Astronautics, The University of Tokyo | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | In this research, cockpit instruments are being developed which aim to offer human pilots longitudinal control advice, considering predicted wind speed ahead. Future wind speed trends can be measured with an onboard Doppler LIDAR system developed by JAXA. Knowing about future wind changes enables the pilot to prepare slowly responding systems such as thrust in advance. This paper proposes a pitch and thrust advisory calculation method and a cockpit display to show the calculated advice to the pilot. Since the proposed system shows control advice to human pilots, it should be designed to be easily usable for them. The energy principle was chosen for the advisory calculation because of its intuitive concept and its ability to integrate thrust and elevator control when calculating the control advice; something which is not possible with the current separated autopilot and auto throttle systems. From the flight dynamics viewpoint, the basic equations of motions and the energy principle theory are extended to deal with the effect of wind when the advisory system calculates the required control inputs. Simulations were carried out to evaluate the advisory calculation with the energy principle and showed appropriate preparation for the expected wind shear is achieved with the LIDAR information. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | The 2016 Asia-Pacific International Symposium on Aerospace Technology (APISAT2016), Toyama, Japan, 25-27 Oct 2016 | |||||
書誌情報 | 発行日 2016 |