Range Prediction Patents (Class 235/416)
-
Patent number: 8788120Abstract: System and methods for managing targets of a vehicle is provided. In some aspects, a system may include a boundary check module configured to receive boundary information from a flight safety system. The boundary information comprises a selected termination boundary of a plurality of termination boundaries confining navigation of the vehicle. Each of the plurality of termination boundaries is associated with a target of a plurality of targets of the vehicle. The system may further include a target modification module configured to select the target associated with the selected termination boundary, and a target guidance module configured to provide the selected target to a guidance and control system of the vehicle.Type: GrantFiled: April 19, 2011Date of Patent: July 22, 2014Assignee: Lockheed Martin CorporationInventors: Andrew P. Imbrie, Steven A. Dunn, Andrew A. Myers
-
Patent number: 8520895Abstract: A system and method calculate a range and velocity of an object in image data. The range calculation includes detecting a contour of the object from the image data, forming a template from the image data based on the contour; and calculating a range to the object using pixel resolution and dimension statistics of the object. A three-dimensional velocity of the object is determined by calculating a radial component and an angular component of the velocity. The radial velocity component is calculated by determining the range of the object in two or more image frames, determining a time differential between the two or more image frames, and calculating the radial velocity as a function of the range of the object in the two or more image frames and the time differential between the two or more image frames. The angular component is calculated using spatial-temporal derivatives as a function of a motion constraint equation.Type: GrantFiled: December 29, 2010Date of Patent: August 27, 2013Assignee: Honeywell International Inc.Inventors: Kwong Wing Au, Saad J. Bedros
-
Patent number: 8459552Abstract: This invention relates to a method, system and computer program product that calculates a real-time, accurate, firing solution for man carried weapon system; specifically a transparent display to be located in-line with a weapon mounted optic and a device to adjust the aim point through real-time data collection, analysis and real-time visual feedback to the operator. A firing solution system mounted on a projectile weapon comprising: A Sensor and CPU Unit (SCU) and a Sight Adjusted Reticule (SAR) and a PC Dongle which configured to facilitate communication between the SCU and a personal computer (PC), or similar computing device, enabling management of the SCU configuration and offloading of sensor obtained and system determined data values.Type: GrantFiled: August 1, 2011Date of Patent: June 11, 2013Assignee: Awis LLCInventor: Paul Arbouw
-
Patent number: 7832137Abstract: The present invention relates to target acquisition and related devices, and more particularly to telescopic gunsights and associated equipment used to achieve shooting accuracy at, for example, close ranges, medium ranges and extreme ranges at stationary and moving targets.Type: GrantFiled: December 28, 2006Date of Patent: November 16, 2010Assignee: Horus Vision, LLCInventors: Dennis J. Sammut, Lawrence Chao, Dickinson Buell
-
Patent number: 5992292Abstract: A fire-control system for anti-aircraft defense systems, particularly mobile ones, having at least one launch apparatus for guided missiles that is pivotable in elevation and disposed on a platform that is pivotable in azimuth, has an optical target-tracking sensor that is rigidly coupled with the launch apparatus, a follow-up computer for panning the target-tracking sensor after targets, a directional angle computer for calculating lead and elevation of the guided missile during launch, and a control unit that has adjustment drives for the platform and launch apparatus, which unit pivots the platform in azimuth and the launch apparatus in elevation, and, prior to launch, locks the lead on the platform and the elevation on the launch apparatus.Type: GrantFiled: March 3, 1994Date of Patent: November 30, 1999Assignee: STN Atlas Elektronic GmbHInventor: Luitjen Ennenga
-
Patent number: 5920027Abstract: A fire control system and a method for estimating periodic component of a target path. An efficient, fast-setting estimator is realized by first estimating the period and then the amplitude of the periodic component on the basis of the most recent measurements made.Type: GrantFiled: August 15, 1997Date of Patent: July 6, 1999Assignee: Hollandse Signaalapparaten B.V.Inventor: Abraham Johannes Maas
-
Patent number: 5635662Abstract: A method and apparatus for use by a personnel in combat unit to assess in bstantially real-time the threat to a combat unit posed by one or more threat projectiles. A command and control system receives a variety of input data and information signals and generates corresponding signals directed to a processing module. The processing module receives and processes the informational signals indicative of the status and characteristics of the combat unit and threat projectile. The processing module determines whether sample threat projectiles with an uncertainty region associated with each threat projectile detects the combat unit and determines therefrom a probability that the actual threat projectile detects the combat unit. The processing module also generates a probability of detection signals, to generate a report in user perceivable form, indicative of the probability of the threat projectile detecting the combat unit on a substantially real-time basis.Type: GrantFiled: February 7, 1996Date of Patent: June 3, 1997Assignee: The United States of America as represented by the Secretary of the NavyInventors: David B. Robertson, Joseph J. Perruzzi, Laura C. Rabenold
-
Patent number: 4671165Abstract: The sighting device comprises first means for displaying at least one displacement mark parallel to the central vertical spider-line, means for altering the position of said displacement mark, means for measuring the target moving time which has elapsed between one initial moment at which the target seen in the range finder is superimposed with a reference mark, and a subsequent moment at which said target seen in the range finder held in immobilized position reaches said displacement mark; and second means for displaying at least one cross velocity adjusted mark, parallel to said central vertical spider-line, and whose position is determined first as a function of the projectile flight time, which is itself determined from the firing distance, and second, as a function of the target moving time, measured for a given displacement mark.Type: GrantFiled: December 21, 1984Date of Patent: June 9, 1987Assignee: Societe Europeenne de PropulsionInventors: Richard Heidmann, Pierre Miquet