Aircraft flight operations datalink
Aircraft flight operations datalink for preparing an aircraft for flight, by a particular pilot (crew) for a particular flight plan via a portable computing device. The aircraft flight operations datalink includes a wireless data link; computer processor; data bus; an association with a flight sensor for collecting aircraft position, weather, traffic, terrain, aircraft systems status, aircraft flight envelope parameters, pilot (crew) status/condition; a display system; a ground-to-air data link; and a database of aircraft and pilot data; a flight plan; and flight conditions. In flight operations, the datalink may be utilized to relieve a pilot (crew) from performing tasks necessary to mitigate an emergency or reduce a flight operation urgency.
1. An aircraft, comprising:
(a) a bus;
(b) at least one sensor connected to said bus to report one or more of a position, airspeed, attitude, or altitude of the aircraft;
(c) an autopilot connected to said bus and one or more aircraft controls, the autopilot capable of directing adjustment of one or more of the position, airspeed, attitude, or altitude via the one or more aircraft controls;
(d) a wireless data-link connected to said bus to receive at least one expected flight path for the aircraft from a portable computing device;
(e) a memory connected to said bus for storing the received expected flight path;
(f) at least one processor connected to said bus and coupled with one or more of the sensor, autopilot, wireless data-link, or memory, the at least one processor programmed to:
receive at least one of a position, airspeed, altitude, or attitude of the aircraft from the at least one sensor;
receive, via a user interface, at least one pilot input including:
(1) a flight control input to adjust one or more of the position, airspeed, altitude, or attitude, the flight control input associated with a deviation of the aircraft from at least one performance norm;
wherein, when the at least one pilot input is a flight control input, the at least one processor is further programmed to:
correct the deviation via the aircraft controls after one or more notifications are provided and the one or more notifications are unacknowledged, wherein the one or more notifications are more insistent as the deviation at least one of persists or increases;
or
(2) a pilot request to correct the deviation of the aircraft; wherein, when the at least one pilot input is a pilot request, the at least one processor is further programmed to correct the deviation via the aircraft controls by initiatinq at least one emergency protocol;
and
create an alternate landing site (ALS) hierarchy by determining a suitability value for each of a plurality of alternate landing sites, wherein each assigned suitability value is based on weighting a plurality of factors related to the alternate landing site's suitability for landing;
and
(g) a display connected to said bus for displaying flight information.
2. The aircraft of claim 1 , wherein said deviation correction is a procedure selected from said memory, said procedure wirelessly updated to said memory via the portable computing device.
3. The aircraft of claim 2 , wherein said memory is a data repository of a portable computing device configured to receive preflight data via said wireless data-link from a second data repository operably coupled to a ground-based computing device.
4. The aircraft of claim 3 , wherein said portable computing device includes at least one of a tablet or a smartphone.
5. The aircraft of claim 1 , wherein: said memory further comprises an onboard dataset to receive one or more updates wirelessly from a portable computing device, the one or more updates associated with at least one of a flight plan parameter, aircraft parameter, pilot parameter, or system parameter.
6. The aircraft of claim 1 , further comprising:
at least one additional processor associated with at least one of said at least one sensor, weather sensor, traffic sensor, wireless data-link, aircraft performance control, autopilot, or annunciator;
wherein said initiation of the deviation correction is distributed between said at least one processor and said at least one additional processor,
and
wherein said annunciator is at least one of a voice notification, graphic display, audio tone, or haptic notification.
7. The aircraft of claim 1 , wherein said display is capable of displaying a turn back for re-landing procedure and the processor is capable of instructing the display to display a re-land procedure when the processor determines the aircraft may re-land based at least in part on at least one of position, airspeed, attitude, or altitude.
8. The aircraft of claim 6 , wherein said aircraft performance control includes at least two of a throttle, elevator, rudder, ailerons, flaps, spoiler, or gear.
9. The aircraft of claim 8 , wherein said display is capable of displaying at least one of angle of attack or aircraft total energy.
10. The aircraft of claim 9 , wherein said display is capable of displaying at least one of aircraft kinetic energy available to convert to potential energy, or aircraft potential energy available to convert to kinetic energy.
11. The aircraft of claim 10 , wherein said processor includes a total energy flight controller.
12. The aircraft of claim 11 , wherein said display at least one of textually or graphically displays information related to said initiated deviation correction.
13. The aircraft of claim 2 , wherein said display at least one of textually or graphically displays one or more items associated with said procedure in seriatim.
14. The aircraft of claim 13 , wherein said display at least one of textually or graphically displays said procedure as a flight director on an artificial horizon.
15. The aircraft of claim 1 , wherein said wireless data-link communicatively connects said portable computing device to an aircraft receiver.
16. The aircraft of claim 1 , wherein said wireless data-link is a wireless data-link to aircraft avionics, and at least one of surface-based or space-based radio.
17. The aircraft of claim 2 , wherein said wireless data-link receives said expected flight path of the aircraft from said portable computing device during at least one of a preflight, a flight, or a postflight of the aircraft.
18. The aircraft of claim 4 , wherein said aircraft parameter further includes at least one of a maintenance status, a catering status or requirement, a potable water and waste status, a temperature or lighting status, or an aircraft requirement.
19. The aircraft of claim 4 , wherein said flight plan parameter further includes a path of connected planned flight fixes including at least one of a navigational aid (navaid), a waypoint, or an airway.
20. The aircraft of claim 4 , wherein said flight plan parameter further includes at least one of a schedule, a route, a load, a fuel plan, a fix list, an overflight authorization, or a notice to air missions (NOTAM).
21. The aircraft of claim 4 , wherein said pilot parameter further includes at least one of a crew member list, a pilot monitor including a flight time limitation, a duty time limitation, a latest allowable takeoff time (LATT), or a pilot schedule.
22. The aircraft of claim 1 , wherein said at least one processor is further programmed for communicating with maintenance at least one of before, during, or after a flight segment.
23. The aircraft of claim 4 , wherein said at least one processor is further programmed for querying at least one of a ground-to-air, air-to-air, or space-based satellite database for said at least one flight plan parameter, aircraft parameter, pilot parameter, or system parameter.
24. The aircraft of claim 1 , wherein said at least one processor is further programmed for sending a notification to the pilot or ground personnel during a preflight assessment.
25. The aircraft of claim 1 , wherein said at least one processor is programmed for informing the pilot of a configuration of the aircraft different from an expected configuration.
26. The aircraft of claim 1 , wherein the weiqhted factors include one or more of
the current position of the aircraft;
an airport landing procedure;
or
at least one additional selection criteria selected from the group including at least one of a weather condition, wind condition, or runway length.
27. The aircraft of claim 1 , wherein said processor selects an alternate landing site from the ALS hierarchy based on the determined suitability values.
28. The aircraft of claim 27 , wherein said processor creates a flight path from a current position of the aircraft to a landing associated with the selected alternate landing site via at least one of a waypoint or an initial approach fix.
29. The aircraft of claim 28 , wherein said processor reports to air traffic control an aircraft diversion.
30. The aircraft of claim 29 , wherein said processor is programmed to:
determine an estimated time of arrival at the selected alternate landing site;
display the selected alternate landing site and a route to the selected alternate landing site on the display;
and
continue to determine the suitability of at least the selected alternate landing site, and reroute the aircraft to a new alternate landing site, based on changes to the determined suitability.