The disclosed embodiments describe collision warning devices, controllers, and computer readable media. A collision warning device for towing vehicles includes a housing, a scanning sensor, a display, and a controller. The housing is configured to be secured to at least one of a tow operator and a tug during aircraft towing operations. The a scanning sensor is secured to the housing and is configured to scan an aircraft and to scan an object in an environment surrounding the aircraft. The controller is mounted to the housing and is operably coupled with the scanning sensor and the display. The controller is configured to generate a three dimensional (3D) model of the aircraft and the environment based on a signal output from the scanning sensor, and to calculate potential collisions between the aircraft and the object based on the 3D model.

The disclosure relates to airport stand arrangement (100,200,300) comprising: a display (130); a radar-based system (110R); and one or more additional systems selected from laser-based systems (110L) and imaging systems (110C), wherein said radar-based system (110R) and said one or more additional systems together form a combined system (110,210,310), wherein the airport stand arrangement (100) is configured, based on output data from said combined system (110), to detect and track (S108,S110) an aircraft (10) within a stand area (20) when said aircraft (10) is approaching a stand within the stand area (20) for parking at a parking position (160) therein, and configured, based on said detection and tracking of the approaching aircraft (10), to provide (S114,S116) pilot maneuvering guidance information on said display (130) for aiding a pilot of the approaching aircraft (10) in maneuvering the aircraft (10) towards said parking position (160).

A computer-implemented method of obtaining an excursion report for an aircraft is disclosed. The aircraft includes one or more sensors and a vision system, and the method includes obtaining sensor data from the one or more sensors; storing and time-stamping the sensor data; operating the vision system to detect the aircraft leaving a runway or taxiway; recording a start time of an excursion period based on a time of detection of the aircraft leaving the runway or taxiway; operating the vision system to detect the aircraft returning to the runway or taxiway; recording an end time of the excursion period based on a time of detection of the aircraft returning to the runway or taxiway; and compiling an excursion report, the excursion report comprising: the start time of the excursion period, the end time of the excursion period and a subset of the sensor data which was time-stamped during the excursion period.

A computer-implemented method of obtaining an excursion report for an aircraft is disclosed. The aircraft includes one or more sensors and a vision system, and the method includes obtaining sensor data from the one or more sensors; storing and time-stamping the sensor data; operating the vision system to detect the aircraft leaving a runway or taxiway; recording a start time of an excursion period based on a time of detection of the aircraft leaving the runway or taxiway; operating the vision system to detect the aircraft returning to the runway or taxiway; recording an end time of the excursion period based on a time of detection of the aircraft returning to the runway or taxiway; and compiling an excursion report, the excursion report comprising: the start time of the excursion period, the end time of the excursion period and a subset of the sensor data which was time-stamped during the excursion period.

A collision avoidance system for an airplane under tow may include a sensing device configured to capture image data of at least a portion of the airplane and an object while the airplane is being towed. The sensing device may be located remotely to both the airplane and the object. Positions of two or more features of the airplane may be determined based on the image data. A bounding box encompassing the airplane may be generated based, at least in part, on the positions of the two or more features. Additionally, based on a comparison of the position of an object relative to the bounding box, it may be determined whether the object is within a predetermined distance from the airplane.

On-board vehicular monitoring system in a movable vehicle including a frame defining a compartment in which an occupant is able to sit and a drive system for enabling movement of the vehicle. The monitoring system includes at least one sound-receiving/vibration-detecting component that receives sounds from an environment in or around the vehicle and/or detects vibration, a processor coupled to each sound-receiving/vibration-detecting component and that analyzes the sounds and/or vibrations to identify non-speech sounds or vibrations, and a communications device coupled to the processor that transmits a signal, data or information about analysis by the processor of the identified non-speech sounds to a remote location separate and apart from the vehicle.

A system for assisting in guiding of an aircraft maneuvered by an aircraft tractor on the ground, the system including at least one projection device including a laser generating a laser beam fixed to an anchor point of the fuselage of the aircraft. A fixing mechanism is configured to fix the projection device to an anchor point of the fuselage, the laser beam from each laser projector then plotting a light trace on the ground to be used to assist in guiding the aircraft on the ground. A camera can film the light trace on the ground. A remote display device includes a screen, the display device being positioned on the aircraft tractor for the screen to be visible to an operator of the aircraft tractor, each projection device being connected to the display device, the display device being configured to display the image from each projection device camera.

A sensor system is described that leverages low power motion sensors to trigger the activation of higher power proximity sensors. The system may be configured to monitor the motion of a vehicle, such as an aircraft in which it is installed. The sensor system may initially start in a dormant state, and once the vehicle is moved, such as when an aircraft is towed, a proximity sensor may be activated, which draws power from a dedicated battery unit. Once the proximity sensor is activated, the sensor system may continue to monitor proximity data generated by the proximity detection system and sound an alarm if the vehicle comes within a threshold distance of some object. The sensor system may also utilize state of the vehicle's electrical system to recharge the battery and/or to disable various components, thereby optimizing power consumption.

A permanent wireless onboard to ground operations communications system is provided for an aircraft equipped with a pilot-controllable drive wheel drive system for autonomous ground movement without reliance on the aircraft's engines or external tow vehicles, including an onboard wireless communications link installed to remain permanently with the aircraft designed to interface wirelessly with ground personnel at any airport, aerodrome, or airfield where the aircraft lands immediately upon landing. The permanent wireless onboard to ground operations communications system provides a substantially instantaneous connection between a pilot and ground personnel to facilitate guidance of pilot-controlled autonomous ground movement during taxi, parking in nose-in and parallel orientations, and pushback without reliance on visual signals. The present communications system establishes and maintains cockpit to ground communications during pilot-controlled autonomous aircraft ground movement to enhance the safety of ramp operations and improve the speed at which ramp operations can be safely conducted.

A flight management system with core and supplementary modules is proposed. The core module may include generic applications that implement generic functionalities related to a flight management of the aircraft. The supplementary module may include supplementary applications that implement supplementary functionalities specific to an entity to which the aircraft belongs. The supplementary module may be divided into principal and auxiliary partitions (or entities), and the supplementary applications, also referred to as principal applications, may be implemented in the principal partition. One or more auxiliary applications may be implemented in the auxiliary partition. Each auxiliary application may be associated with one or more principal applications such that the execution of the principal application requires the associated auxiliary application to be executed.