发明名称 DISPLAY DEVICE, PILOTING ASSISTANCE SYSTEM, AND DISPLAY METHOD
摘要 An FPM (30) and a target air attitude angle indication (32) are displayed on a PFD (10) which is an integrated instrument. The target air attitude angle indication (32) is an index showing a target angle of attack and a target air attitude angle, said target angle of attack being an angle of attack that is set as a target for the purpose of reaching a target flight path of an aircraft being piloted, and said target air attitude angle serving to show a target sideslip angle which is a sideslip angle that is set as a target. The PFD (10) displays the relative difference between the FPM (30) and the target air attitude angle indication (32), and the matching (overlapping) of the FPM (30) with the target air attitude angle indication (32) indicates that the aircraft being piloted is flying along a target travel direction. Due to the above, piloting with better path following performance than in the case of piloting based on a target ground attitude angle becomes possible.
申请公布号 WO2012002276(A1) 申请公布日期 2012.01.05
申请号 WO2011JP64539 申请日期 2011.06.24
申请人 MITSUBISHI HEAVY INDUSTRIES, LTD.;THE SOCIETY OF JAPANESE AEROSPACE COMPANIES;YAMASAKI, KOICHI 发明人 YAMASAKI, KOICHI
分类号 B64D45/00;G08G5/00 主分类号 B64D45/00
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