초록 ▼

Device assisting with interception by an aircraft of a flight path segment located in a horizontal plane and a system of assistance with interception and follow-up of such a segment. The device includes means of determining a ground speed vector and means of displaying to present, on a screen, a mea

Device assisting with interception by an aircraft of a flight path segment located in a horizontal plane and a system of assistance with interception and follow-up of such a segment. The device includes means of determining a ground speed vector and means of displaying to present, on a screen, a means of indication (10) of the ground speed corresponding to a first rectilinear section (10) in the horizontal plane, connected to a symbol (7) whose angular orientation corresponds to the direction of said ground speed vector and whose length is variable, a means of interception approach indication (12) corresponding to a second recipient section (3) in the horizontal plane of variable width and provided for as an extension of first rectilinear section (11) and a means of indication (14) of the interception turn corresponding to at least one circle arc (15) in the horizontal plane, provided to extend second rectilinear section (13).

대표청구항 ▼

The invention claimed is: 1. A method for assisting a pilot to fly an airplane to intercept a flight path, the method comprising the steps of: calculating a ground speed vector of the airplane; displaying on a display screen in the airplane a representation of the flight path; displaying on the dis

The invention claimed is: 1. A method for assisting a pilot to fly an airplane to intercept a flight path, the method comprising the steps of: calculating a ground speed vector of the airplane; displaying on a display screen in the airplane a representation of the flight path; displaying on the display screen a first symbol representing a position of the airplane relative to the flight path; displaying on the display screen a first indicator that is attached to said first symbol and that is a straight line with an angular orientation corresponding to a direction of the ground speed vector and with a length that varies and corresponds to a magnitude of the ground speed vector when the magnitude exceeds a predetermined value and that is constant and proportional to the predetermined value when the magnitude is less than or equal to the predetermined value; displaying on the display screen a second indicator that is attached to said first indicator and that is a straight line whose direction represents an initial part of a future approach path for the airplane to intercept the flight path and whose length adjusts as the position of the airplane changes relative to the flight path; and displaying on the display screen a third indicator that extends tangentially from said second indicator and that is connected tangentially to the flight path, said third indicator being a curved line representing a final part of the future approach path for intercepting the flight path, wherein the flight path to be intercepted and the first, second, and third indicators are displayed on the screen at the same time. 2. The method of claim 1, further comprising the step of delaying the display of the second and third indicators on the display screen until the direction of the ground speed vector intercepts the flight path and until the airplane is less than a predetermined distance from the flight path. 3. The method of claim 1, further comprising the step of making a curvature of said third indicator depend on at least one of an airspeed of the airplane, a turning capability of the airplane, and wind speed and direction. 4. The method of claim 1, further comprising the step of delaying the display of said third indicator until a curvature of said third indicator is achievable by the airplane. 5. The method of claim 1, further comprising the steps of detecting an obstacle and displaying on the display screen a second symbol representing a relative position of the detected obstacle. 6. The method of claim 1, further comprising the step of transmitting flight information for intercepting the flight path to an autopilot that controls movement of the airplane, the flight information being based on the first, second, and third indicators. 7. The method of claim 1, further comprising the step of providing said third indicator with two parts, a first one of said two parts being a curved line extending tangentially from said second indicator and crossing the flight path and a second one of said two parts being a curved line extending tangentially from said first part and being connected tangentially to the flight path. 8. The method of claim 1, wherein the method further assists the pilot to fly the airplane to follow the flight path after the airplane has intercepted the flight path, and further comprises the steps of: calculating a lateral deviation of the airplane from the flight path and tolerated lateral margins on both sides of the flight path, wherein said first symbol indicates the lateral deviation of the airplane from the flight path by a relative position of said first symbol to said flight path; displaying on the display screen a lateral deviation scale; and displaying on the display screen an excessive lateral deviation marker when the airplane is approaching one of said tolerated lateral margins. 9. The method of claim 8, further comprising the step of automatically adjusting a distance indicated by said lateral deviation scale as a flight corridor width defined by said tolerated lateral margins changes. 10. The method of claim 8, further comprising the step of displaying on the display screen slanted lines indicating a change in a width of a flight corridor defined by said tolerated lateral margins. 11. The method of claim 8, further comprising the step of displaying on the display screen a lateral drift indicator that represents a lateral drift speed of the airplane, said lateral drift indicator being attached to said first symbol and varying in length in proportion to the lateral drift speed.