View source for 17958151. LANDING GUIDANCE FOR AIR VEHICLES USING NEXT GENERATION CELLULAR NETWORKS simplified abstract (Honeywell International Inc.)

=LANDING GUIDANCE FOR AIR VEHICLES USING NEXT GENERATION CELLULAR NETWORKS=


==Organization Name==

[[:Category:Honeywell International Inc.|Honeywell International Inc.]]


[[Category:Honeywell International Inc.]]

==Inventor(s)==

[[:Category:Willard R. True of Kirkland WA (US)|Willard R. True of Kirkland WA (US)]][[Category:Willard R. True of Kirkland WA (US)]]

[[:Category:Donald C. Kauffman of Laurel MD (US)|Donald C. Kauffman of Laurel MD (US)]][[Category:Donald C. Kauffman of Laurel MD (US)]]

==LANDING GUIDANCE FOR AIR VEHICLES USING NEXT GENERATION CELLULAR NETWORKS - A simplified explanation of the abstract==


This abstract first appeared for US patent application 17958151 titled 'LANDING GUIDANCE FOR AIR VEHICLES USING NEXT GENERATION CELLULAR NETWORKS

==Simplified Explanation==

The landing guidance system described in the patent application involves using edge nodes in a mobile communications network to provide landing guidance information to an air vehicle. This information is generated based on location information received from the network location management function and is transmitted to the air vehicle when it meets a reliability threshold. The processor onboard the air vehicle then uses this guidance information to guide the vehicle to the landing target area.

* Edge nodes in a mobile communications network communicate with an air vehicle's processor to provide landing guidance information.
* The landing guidance information is generated based on location information from the network location management function.
* The information is transmitted to the air vehicle when it meets a reliability threshold.
* The air vehicle's processor guides the vehicle to the landing target area using the provided guidance information.

== Potential Applications ==
The technology can be applied in autonomous landing systems for drones, helicopters, and other air vehicles.

== Problems Solved ==
This technology solves the problem of providing accurate and reliable landing guidance information to air vehicles, improving safety and efficiency during landings.

== Benefits ==
The benefits of this technology include enhanced precision in landing procedures, reduced human error, and increased overall safety during landing operations.

== Potential Commercial Applications ==
Commercial applications of this technology include use in the aviation industry for automated landing systems in both manned and unmanned aircraft.

== Possible Prior Art ==
One possible prior art for this technology could be existing landing guidance systems used in aviation, such as Instrument Landing Systems (ILS) or Global Positioning System (GPS) based landing systems.

=== Unanswered Questions ===

=== How does the system handle communication disruptions between the edge nodes and the air vehicle's processor? ===
The patent application does not provide details on how the system manages communication disruptions between the edge nodes and the air vehicle's processor. This is an important aspect to consider, especially in scenarios where reliable communication is crucial for safe landing operations.

=== What measures are in place to ensure the security and integrity of the landing guidance information transmitted to the air vehicle? ===
The patent application does not address the security and integrity of the landing guidance information transmitted to the air vehicle. It is essential to understand the security measures in place to prevent unauthorized access or tampering with the guidance information, which could potentially compromise the safety of the landing operation.


==Original Abstract Submitted==

A landing guidance system comprises at least one edge node that operatively communicates with a mobile communications network, wherein the mobile communications network includes a network location management function, and at least one processor onboard an air vehicle, the at least one processor in operative communication with the edge node. The at least one edge node is operative to provide landing guidance information to the air vehicle by a method that comprises receiving location information from the network location management function; generating the landing guidance information for the air vehicle based on the location information; and transmitting the landing guidance information to the air vehicle when the landing guidance information meets a reliability threshold. The at least one processor is operative to guide the air vehicle to the landing target area using the landing guidance information.



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