飛行推進統合制御対応航空エンジン制御装置の研究　　第２報：飛行推進統合制御

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書誌事項

タイトル別名
  • A Study on Aircraft Engine Control Systems for Integrated Flight and Propulsion Control Part 2: Integrated Flight and Propulsion Control
  • ヒコウ スイシン トウゴウ セイギョ タイオウ コウクウ エンジン セイギョ ソウチ ノ ケンキュウ ダイ2ホウ ヒコウ スイシン トウゴウ セイギョ
  • A Study on Aircraft Engine Control Systems for Integrated Flight and Propulsion Control
  • Part 2: Integrated Flight and Propulsion Control
  • 第2報：飛行推進統合制御

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The Integrated Flight and Propulsion Control (IFPC) for a highly maneuverable aircraft and a fighter-class engine with pitch/yaw thrust vectoring is described. Of the two IFPC functions the aircraft maneuver control utilizes the thrust vectoring based on aerodynamic control surfaces/thrust vectoring control allocation specified by the Integrated Control Unit (ICU) of a FADEC (Full Authority Digital Electronic Control) system. On the other hand in the Performance Seeking Control (PSC) the ICU identifies engine's various characteristic changes, optimizes manipulated variables and finally adjusts engine control parameters in cooperation with the Engine Control Unit (ECU). It is shown by hardware-in-the-loop simulation that the thrust vectoring can enhance aircraft maneuverability/agility and that the PSC can improve engine performance parameters such as SFC (specific fuel consumption), thrust and gas temperature.

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