Abstract: Provided are technologically improved systems and methods for providing terrain and runway feedback for an aircraft over a secured datalink. The method utilizes a controller onboard the aircraft and one on the ground. The controller onboard the aircraft performs the operations of: formatting a data package of mobile platform data; confirming the aircraft has a valid subscription service; securing the data package using a security protocol; and transmitting the data package via a secured datalink. The ground controller performs the operations of: confirming the subscription service of the aircraft; validating the security protocol used on the data package; decoding and processing the data with map extraction, threat detection, and image generation to generate raw terrain and runway feedback data; and transmitting the raw data using the secured datalink. An alert controller is used to generate alert commands for various alert devices based on the raw terrain and runway feedback data.

Abstract: Provided are technologically improved systems and methods for providing terrain and runway feedback for an aircraft over a secured datalink. The method utilizes a controller onboard the aircraft and one on the ground. The controller onboard the aircraft performs the operations of: formatting a data package of mobile platform data; confirming the aircraft has a valid subscription service; securing the data package using a security protocol; and transmitting the data package via a secured datalink. The ground controller performs the operations of: confirming the subscription service of the aircraft; validating the security protocol used on the data package; decoding and processing the data with map extraction, threat detection, and image generation to generate raw terrain and runway feedback data; and transmitting the raw data using the secured datalink. An alert controller is used to generate alert commands for various alert devices based on the raw terrain and runway feedback data.

Abstract: Systems and methods are operable to identify and indicate opportunities for an In-Trail procedure (ITP) aircraft to make an ITP altitude change. An exemplary embodiment receives information corresponding to a desired ITP altitude for the ITP aircraft and a projected window period; estimates at least one ITP maneuver opportunity window based on the estimated location of each of the plurality of other aircraft and based on a current airspeed and a current altitude of the ITP aircraft; generates a screen shot that presents an ITP maneuver opportunity window icon, wherein the ITP maneuver opportunity window icon graphically indicates the soonest time and the latest time that the ITP aircraft may initiate the ITP maneuver, and wherein the ITP maneuver opportunity window icon indicates an altitude change made by the ITP aircraft will maintain minimum safe self-separation distances from the plurality of other aircraft during the ITP maneuver.

Abstract: Systems and methods are operable to identify and indicate opportunities for an In-Trail procedure (ITP) aircraft to make an ITP altitude change. An exemplary embodiment receives information corresponding to a desired ITP altitude for the ITP aircraft and a projected window period; estimates at least one ITP maneuver opportunity window based on the estimated location of each of the plurality of other aircraft and based on a current airspeed and a current altitude of the ITP aircraft; generates a screen shot that presents an ITP maneuver opportunity window icon, wherein the ITP maneuver opportunity window icon graphically indicates the soonest time and the latest time that the ITP aircraft may initiate the ITP maneuver, and wherein the ITP maneuver opportunity window icon indicates an altitude change made by the ITP aircraft will maintain minimum safe self-separation distances from the plurality of other aircraft during the ITP maneuver.

Abstract: Systems and methods are operable to present graphical information indicating capability of an aircraft to change altitude. An exemplary embodiment determines an altitude change capability of the aircraft; determines an altitude change capability icon based on the determined altitude change capability of the aircraft, wherein the altitude change capability icon is defined by at least a leading portion, a trailing portion, a top portion, and a bottom portion, wherein a slope of the leading portion of the altitude change capability icon corresponds to the determined altitude change capability of the aircraft, and wherein the leading portion and the trailing portion are separated by at least the top portion and the bottom portion; and communicates the altitude change capability icon to a display for presentation to the crew of the aircraft.

Abstract: Systems and methods are operable to present graphical information indicating capability of an aircraft to change altitude. An exemplary embodiment determines an altitude change capability of the aircraft; determines an altitude change capability icon based on the determined altitude change capability of the aircraft, wherein the altitude change capability icon is defined by at least a leading portion, a trailing portion, a top portion, and a bottom portion, wherein a slope of the leading portion of the altitude change capability icon corresponds to the determined altitude change capability of the aircraft, and wherein the leading portion and the trailing portion are separated by at least the top portion and the bottom portion; and communicates the altitude change capability icon to a display for presentation to the crew of the aircraft.