Exelis Inc.

Christopher T Rodgers

Omid Ebrahimi Kia

Javier Mendez-Rodriguez

Brian Bradford

A system is provided for alerting a crew in an airborne platform. The system includes a module for receiving point cloud data from a LIDAR system, including range data between the LIDAR system and multiple points in the point cloud. The system also includes a module for placing the multiple points into first and second zones, wherein the first zone has range data of points in the point cloud located within a first distance from the airborne platform, and the second zone has range data of points located further than the first distance. The first distance is predetermined by an operational environment of the airborne platform. The system further includes a color module for coloring the points in the first zone with a first color composition and coloring the points in the second zone with a second color composition. A color display is provided for displaying the colored points in the first and second zones.

Point cloud visualization using bi-modal color schemes based on 4D lidar datasets

A method for collecting data of species in the magnetosphere includes the steps of: (a) tuning at least one laser to spectral indices of targeted atomic or molecular species located in the magnetosphere; and (b) measuring fluorescence radiation from each of the targeted species, in response to the tuning step. The method determines range to each of the targeted species. The method geo-locates the species with respect to the Earth to provide a registered map of the targeted species in three dimensions (3D) with respect to the Earth; and temporally trends each of the targeted species to provide the registered map in four dimensions (4D). The method may also determine abundance from multiple wavelengths returned from the fluorescence radiation of the targeted species.

System and method of visualization of species characterization, dynamics and stratification of the magnetosphere

A system for identifying at least one species in space includes a physical response module for outputting multiple spectral data based on received signals from a target in space; a calibration module for receiving the spectral data and outputting a first dataset, including density of an {x, y, z} coordinate location in space as a function of time, t; and a classification module for receiving the first dataset, and outputting a second dataset including multiple tuples of {x, y, z, t, d} associated with the at least one species, wherein d is density of the at least one species. Also included is an HD processor for receiving the second dataset from the classification module and providing a visual image of the second dataset to a user.

A processor calculates a safe landing zone for an aircraft. The processor executes the following steps: (a) converting 4D point cloud data into Cartesian coordinates to form a height map of a region; (b) segmenting the height map to form boundaries of an object in the region; and (c) determining maximum height within the boundaries of the object. Also included are (d) determining if the maximum height is greater than a predetermined height to form a vertical obstruction (VO) in the region; and (e) determining if the VO is in the line of sight (LOS) of the aircraft to classify the landing zone as safe or unsafe. The processor further includes the step of: (f) forming a slope map over the height map.

Point cloud visualization of acceptable helicopter landing zones based on 4D LIDAR

Systems and methods for detecting objects and weather in space are disclosed. A system for detecting an object in space and space weather includes at least one spacecraft, at least one radiation source, at least one detector, and a controller. The at least one radiation source and the at least one detector are coupled to the at least one spacecraft. The at least one radiation source is configured to transmit a signal. The at least one detector is configured to detect the signal. The signal may be reflected from an object in space. The controller is coupled to the spacecraft and is in communication with the plurality of detectors. The controller is programmed to calculate either a relative position of the object based or a plasma parameter in a region traversed by the signal based on the detected signal.

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Adamstown, MD, United States of America

Christopher T Rodgers