A method is provided that includes generating a visual environment for interactive development of a machine learning (ML) model. The method includes accessing observations of data each of which includes values of independent variables and a dependent variable, and performing an interactive exploratory data analysis (EDA) of the values of a set of the independent variables. The method includes performing an interactive feature construction and selection based on the interactive EDA, and in which select independent variables are selected as or transformed into a set of features for use in building a ML model to predict the dependent variable. The method includes building the ML model using a ML algorithm, the set of features, and a training set produced from the set of features and observations of the data. And the method includes outputting the ML model for deployment to predict the dependent variable for additional observations of the data.

Methods and systems are provided for runway overrun alerts for an aircraft using manually entered parameters for a non-standard runway. The method includes accessing an interface for an enhanced ground proximity warning system (EGPWS). The following parameters are then manually entered: identification of the non-standard runway; a displaced threshold of the non-standard runway; surface conditions of the non-standard runway; a declared length of the non-standard runway; and availability of thrust reversers on the aircraft. The parameters for the aircraft to safely land and stop on the non-standard runway are calculated with the EGPWS. An alert with the EGPWS is generated if the stopping point of the aircraft is near or beyond the end of the non-standard runway.

An aircraft enhanced vision system includes an electromagnetic sensor comprising at least one group of transmitters and at least one group of receivers. The electromagnetic sensor includes a waveform generation assembly powering each transmitter in order to generate the transmitted signal and a signal capture assembly to capture the signal received by each receiver after reflection off of the ground. The transmitters are distinct and spaced apart from the receivers, being arranged so as to form at least one virtual transmitter/receiver network extending in an elongation direction perpendicular to the observation direction from each transmitter/receiver combination between the group of transmitters and the group of receivers.

Systems and methods for displaying a scorecard for rating pilot performance by registering a wearable device based on the identification of the wearable device through pilot profile data, location data, and an identification key data received from the wearable device; linking, the wearable device to the avionic system to receive flight data, and to a cloud server to receive computed performance scores for in-flight display by the wearable device; alternately, in response to a manual input action, authenticating pilot identity to enable pilot access and linking of the flight data to the cloud server for display; generating a set of flight components via a model specified for a flight phase based on data from the wearable device if available, and the flight data, the model includes flight performance score values; displaying a flight phase performance score; and displaying on the graphical user interface in a cockpit display the performance scorecard.

The present disclosure relates to system(s) and method(s) for verifying data loading requirements of an avionics unit. The system receives a request for data loading. The request comprises file data, and data loading requirements associated with the avionics unit. Further, the system obtains target file from a repository based on an analysis of the request. The system further generates valid data set and invalid data set in the target file based on an analysis of the data loading requirements. Upon generation, the system verifies predefined data loading requirements of the avionics unit using the invalid data set from the target file.

A system and method for displaying dynamic time-based ranging over a moving map determines position, heading, and airspeed information of an ownship. Based on the positioning information of the ownship, the moving map projects the ownship forward in time and superimposes on the moving map (which may already include distance-based ranging information) time-based ranging information indicating a projected range of positions of the ownship at future or subsequent times relative to the current time. The displayed time-based ranging indicators may be arcuate in shape but adjusted to account for dynamic factors such as headwinds or tailwinds that may affect the time required for the ownship to reach a target at a given distance.

A system and method for landing an electric aircraft is provided. The system includes a controller, wherein the controller is communicatively connected to the sensor, wherein the controller is configured to, receive a plurality of measured flight data, determine a descent confirmation as a function of the plurality of measured flight data, generate a descent instruction set as a function of the descent confirmation and the plurality of measured flight data, wherein generating the descent instruction set further includes generating a transition instruction set, and transmit the descent instruction set to a plurality of flight components, wherein each flight component of the plurality of flight components are coupled to the electric aircraft.

Disclosed are methods, systems, and non-transitory computer-readable media for detecting wind shear conditions in an urban airspace. For instance, the method may include obtaining aircraft information related to an aircraft in the urban airspace, accessing three-dimensional building information corresponding to the airspace, obtaining wind speed and direction data from a plurality of sensors provided about the airspace, and detecting wind shear conditions in at least a portion of the airspace based on the obtained wind speed and direction data. The method may further include determining real-time flight safety parameters in the portion of the airspace based on the wind shear conditions detected in at least the portion of the airspace, analyzing the determined real-time flight safety parameters along a designated flight path through the portion of the airspace to determine whether an unsafe flight condition exists, and transmitting the analysis to the aircraft or a remote operating station.

Methods and systems for providing landing area information on an active avionic display on a display device in a cockpit of an aircraft. The system includes an avionic display module configured to render an avionic display on a display device; and a landing area guidance module configured to: construct a graphical insert that is smaller than the avionic display, the graphical insert depicting the landing area environment as a two-dimensional area that includes a landing location rendered therein in a first visualization scheme; overlay the graphical insert on a small portion of the avionic display; indicate a target exit on the landing location; determine whether a runway overrun awareness alerting system (ROAAS) alert has been received; determine whether a surface indication alerts (SurfIA) alert has been received; responsive to the ROAAS alert and the SurfIA alert, alter the rendering within the graphical insert.

An aircraft flight attitude display device includes a central processing unit (CPU), a display unit electrically connected to the CPU for showing an aircraft image therein, a flight data receiver unit electrically connected to the CPU, a sky obstacle data receiver unit electrically to the CPU, a ground obstacle data receiver unit electrically connected to the CPU, and a power supply unit electrically connected to the CPU. With these arrangements, the aircraft flight attitude display device aids a pilot in making quick and correct judgment about the aircraft flight attitude relative to the sky and the ground, so as to upgrade the aviation safety.