The invention discloses a novel synthetic vision display method, which comprises the following steps of: switching a
visual angle based on a
ground speed and a
drift angle of a helicopter, providing asynthetic vision image taking a course as the
visual angle when the helicopter is on the ground, providing a synthetic vision image of a transition
visual angle when a take-off
climb exceeds a set speed value, and providing a synthetic vision image of a transition visual angle when the speed is continuously increased to exceed an optimal
climb speed, providing a synthetic visual image taking theflight path as a visual angle; when the
drift angle is too large, switching the synthetic view into a transition
view angle and a course
view angle; when the speed is reduced to approach, switching toa course visual angle; at the moment, if the flight path angle of the helicopter exceeds the standard approach angle, the display position of the horizontal position indicator descends, and the attitude
pitch scale display is wider in range. According to the method, the synthetic visual image with a proper visual angle is displayed according to the
ground speed and the
drift angle of the helicopter, and the display position and the pitching scale display range of the horizontal position indicator are automatically adjusted according to the flight path angle of the helicopter, so that the flight environment is coordinated with the synthetic visual image.