Systems and methods providing assist-to-land and emergency land functions
Flight guidance methods, systems, and aircraft systems providing assist-to-land and emergency land (EL) functions. The method includes generating a visual indication of the availability and status of an assist-to-land function and an EL function when the current altitude of the aircraft exceeds an altitude threshold. When in assist-to-land, visual and audible flight guidance can be generated to guide the pilot to a safe landing at a selected runway or at a best runway for the conditions. Functions can be activated by user manipulations of interface objects and/or by software determinations. Software determinations to enter the EL function can automatically control the flying of the aircraft along an approach profile to a safe landing at a nearest suitable airport. EL determinations can be made based on pilot incapacitation.
1. A flight guidance system for an aircraft, comprising:
a source of aircraft status data;
a display device configured to render an avionic display showing a location and trajectory of the aircraft;
a source configured to provide an emergency land (EL) activate command; and
a controller architecture operationally coupled to the source of aircraft status data, the display device, and the source configured to provide the emergency land (EL) activate command, the controller architecture programmed by programming instructions to:
begin an EL function responsive to the EL activate command, the EL activate command being automatically generated responsive to detecting a lack of pilot response to a prompt for a tailorable threshold of time;
while in the EL function, perform the operations of:
selecting a nearest suitable airport and associated route;
actively controlling an automatic pilot (AP) and an auto-thrust (AT) system to fly the aircraft along the route to a final approach fix;
automatically communicating with air traffic control (ATC);
automatically configuring the aircraft for landing; and
automatically landing the aircraft at the nearest suitable airport; and
control a rudder to keep the aircraft aligned with a runway centerline, as part of a safe landing.
2. The system of claim 1 , wherein the controller architecture is further programmed to automatically configure the aircraft for landing by controlling a flap deployment by digitally manipulating a flap/flap handle at appropriate points along an approach profile of the route.
3. The system of claim 1 , wherein the controller architecture is further programmed to communicate with the ATC by:
commanding the avionics display to automatically change a transponder code to 7700; and
sending datalink messages to the ATC with automated messaging including regular updated position reports, an updated airport destination, and a time to arrival.
4. The system of claim 1 , wherein the controller architecture is further programmed to:
control flare maneuvers during the safe landing; and
the safe landing includes aligning the aircraft with a runway heading prior to touchdown.
5. A flight guidance method for an aircraft comprising:
at a controller architecture comprising a processor, performing the operations of:
receiving aircraft status data;
commanding a display device to render an avionic display showing a location and trajectory of the aircraft;
receiving an activate an emergency land (EL) activate command;
beginning an EL function responsive to the EL activate command, the EL activate command being automatically generated responsive to detecting a lack of pilot response to a prompt for a tailorable threshold of time;
while in the EL function, performing the operations of:
selecting a nearest suitable airport and associated route;
actively controlling an automatic pilot (AP) and an auto-thrust (AT) system to fly the aircraft along the route to a final approach fix;
automatically communicating with air traffic control (ATC);
automatically configuring the aircraft for landing; and
automatically landing the aircraft at the nearest suitable airport; and
controlling a rudder to keep the aircraft aligned with a runway centerline, as part of a safe landing.
6. The method of claim 5 , further comprising automatically configuring the aircraft for landing by controlling a flap deployment by digitally manipulating a flap/flap handle at appropriate points along an approach profile of the route.
7. The method of claim 5 , further comprising:
commanding the avionics display to automatically change a transponder code to 7700; and
sending datalink messages to the ATC with automated messaging including regular updated position reports, an updated airport destination, and a time to arrival.
8. The method of claim 5 , further comprising:
controlling flare maneuvers during the safe landing; and
the safe landing includes aligning the aircraft with a runway heading prior to touchdown.
9. A flight guidance system for an aircraft, comprising:
at least one processor; and
at least one memory communicatively coupled to the at least one processor, the at least one memory comprising instructions that upon execution by the at least one processor, cause the at least one processor to
receive aircraft status data;
command a display device to render an avionic display showing a location and trajectory of the aircraft;
receive an activate an emergency land (EL) activate command;
begin an EL function responsive to the EL activate command, the EL activate command being automatically generated responsive to detecting a lack of pilot response to a prompt for a tailorable threshold of time;
while in the EL function, performing the operations of:
selecting a nearest suitable airport and associated route;
actively controlling an automatic pilot (AP) and an auto-thrust (AT) system to fly the aircraft along the route to a final approach fix;
automatically communicating with air traffic control (ATC);
automatically configuring the aircraft for landing; and
automatically landing the aircraft at the nearest suitable airport; and
controlling a rudder to keep the aircraft aligned with a runway centerline, as part of a safe landing.
10. The system of claim 9 , wherein the at least one memory comprises further instructions that upon execution by the at least one processor, cause the at least one processor to automatically configure the aircraft for landing by controlling a flap deployment by digitally manipulating a flap/flap handle at appropriate points along an approach profile of the route.
11. The system of claim 9 , wherein the at least one memory comprises further instructions that upon execution by the at least one processor, cause the at least one processor to:
command the avionics display to automatically change a transponder code to 7700; and
send datalink messages to the ATC with automated messaging including regular updated position reports, an updated airport destination, and a time to arrival.
12. The system of claim 9 , wherein the at least one memory comprises further instructions that upon execution by the at least one processor, cause the at least one processor to:
control flare maneuvers during the safe landing; and
the safe landing includes aligning the aircraft with a runway heading prior to touchdown.