Safe speed advisories for flight deck interval management (FIM) paired approach (PA) systems
Technologically improved Flight Deck Interval Management Paired Approach (FIMPA) system and methods are provided that provide safe speed guidance to a trail aircraft. The FIMPA system comprises a processor operatively coupled to a memory and a database of aircraft-specific parameters. The processor is configured to: receive instantaneous target traffic state data; receive instantaneous state data of a trail aircraft; process the state data, target traffic state data, and aircraft-specific parameters to determine a safe speed zone to perform paired approach, and a recommended speed; render, on a cockpit display, a paired approach bar (PAB) with indicators for (i) a current location of the target traffic, (ii) a current trail aircraft speed, and (iii) the recommended speed; and wherein the indicators are separate and visually distinguishable from each other; determine a wake risk area; and render the wake risk area in a visually distinguishable manner on the PAB.
1. A method for a paired approach (PA) procedure in a trail aircraft, the method comprising:
receiving instantaneous target traffic state data from an automatic dependent surveillance-broadcast;
receiving instantaneous state data of the trail aircraft from a navigation system;
obtaining aircraft-specific parameters;
processing the state data of the trail aircraft, target traffic state data, and aircraft-specific parameters to determine a safe speed zone for the trail aircraft to perform a paired approach with a target aircraft, and a recommended speed for the trail aircraft;
rendering, on a display system, a paired approach bar (PAB) defined, in part, by visually distinguishing each of:
flight identifying text for the target aircraft;
a PAB safe trail aircraft speed range extending from above a trail aircraft minimum safe speed to a trail aircraft maximum speed;
a current trail aircraft speed;
the recommended speed for the trail aircraft; and
a wake risk area caused by the target aircraft, the wake risk area being a range of trail aircraft speeds below the safe speed zone and above a trail aircraft minimum speed.
2. The method of claim 1 , wherein target traffic state data comprises a four-dimensional (4D) trajectory.
3. The method of claim 2 , wherein aircraft-specific parameters comprise aircraft-specific parameters for the trail aircraft and aircraft-specific parameters for the target aircraft.
4. The method of claim 3 , further comprising:
visually distinguishing, on the PAB, the maximum speed of the trail aircraft.
5. The method of claim 4 , further comprising visually indicating on the PAB, the trail aircraft minimum speed, the trail aircraft minimum speed being associated with an engine stall of the trail aircraft.
6. The method of claim 5 , further comprising visually indicating on the PAB the trail aircraft minimum safe speed.
7. The method of claim 6 , further comprising rendering, next to the flight identifying text for the target aircraft, a symbol for a vertical component of movement of the target aircraft, wherein the vertical component of movement of the target aircraft is one of (i) ascending, (ii) descending, and (iii) holding level.
8. A system for flight interval management paired approach (FIMPA), the system comprising:
a database comprising aircraft-specific parameters;
a memory; and
a processor operatively coupled to the memory and the database, the processor configured to:
receive instantaneous target traffic state data;
receive instantaneous state data of a trail aircraft;
process the state data of the trail aircraft, target traffic state data, and aircraft-specific parameters to determine a safe speed zone for the trail aircraft to perform a paired approach with a target aircraft, and a recommended speed for the trail aircraft;
render, on a display system, a paired approach bar (PAB) defined, in part, by visually distinguishing each of:
flight identifying text for the target aircraft;
a PAB safe trail aircraft speed range extending from above a trail aircraft minimum safe speed to a trail aircraft maximum speed;
a current trail aircraft speed; and
the recommended speed for the trail aircraft; and
a wake risk area caused by the target aircraft, the wake risk area being a range of trail aircraft speeds below the safe speed zone and above a trail aircraft minimum speed.
9. The system of claim 8 , wherein the processor is further configured to: obtain, from the database, aircraft-specific parameters for the trail aircraft and aircraft-specific parameters for the target aircraft.
10. The system of claim 9 , wherein the processor is further configured to render next to the flight identifying text for the target aircraft a symbol for a vertical component of movement of the target aircraft, wherein the vertical component of movement of the target aircraft is one of (i) ascending, (ii) descending, and (iii) holding level.
11. The system of claim 10 , wherein target traffic state data comprises a four dimensional (4D) trajectory.
12. The system of claim 11 , wherein the processor is further configured to render, on the PAB, a visual indication of the trail aircraft maximum speed.
13. The system of claim 12 , wherein the processor is further configured to render, on the PAB, an indicator for the minimum speed of the trail aircraft, the minimum speed being associated with an engine stall.
14. The system of claim 13 , wherein the processor is further configured to render, on the PAB, a visual indication of the trail aircraft minimum safe speed.
15. The system of claim 14 , wherein the processor is further configured to render the current trail aircraft speed in red upon determining that the current trail aircraft speed is below the minimum safe speed.