Display apparatus, control support system, and display method

摘要

A flight path maker (FPM) and a target attitude relative to air display are displayed on a primary flight display (PFD), which is an integrated indicator. The target attitude relative to air display is a mark indicating a target attitude relative to air representing a target angle-of-attack and a target sideslip angle of the aircraft to achieve a target flight path. The PFD displays the relative difference between the FPM and the target attitude relative to air display and shows that the aircraft is flying in the target traveling direction when the FPM matches (is superposed on) the target attitude relative to air display. Thus, controlling with higher trackability than controlling performed based on a target attitude relative to ground is enabled.

主权项

1. A control support system including a sensor section that measures current information about flight in an airplane, which is an aircraft, an autopilot section that derives required information such that the aircraft can fly in a target flight path, and a display apparatus that displays a flying situation of the aircraft, the control support system comprising:
a controller including:
a target angle-of-attack deriving section that derives a target angle-of-attack of the aircraft to achieve the target flight path on the basis of a pitch angle measured by the sensor section and a path angle which is an angle between a horizontal plane and a target traveling direction of the aircraft and which is derived by the autopilot section;a target sideslip angle deriving section that derives a target sideslip angle of the aircraft to achieve the target flight path on the basis of a direction angle measured by the sensor section and a direction angle of the target traveling direction derived by the autopilot section; anda display control section that causes the display apparatus to display a relative difference between a target attitude relative to air, representing the target angle-of-attack that has been derived and the target sideslip angle that has been derived, and a current attitude relative to air, representing a current angle-of-attack and a current sideslip angle of the aircraft.