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60 results about "Navigational system" patented technology

• NAVIGATIONAL SYSTEM (noun) The noun NAVIGATIONAL SYSTEM has 1 sense: 1. a system that provides information useful in determining the position and course of a ship or aircraft. Familiarity information: NAVIGATIONAL SYSTEM used as a noun is very rare. Dictionary entry details.

Computationally efficent radar processing method and sytem for SAR and gmti on a slow moving platform

A method and system for processing radar data obtained from a platform which is subjected to non-uniform movement, the distance the platform travels during the formation of an image comprising an aperture; the system comprising software programming for performing a subroutine for building up an average pulse representing a single point on the aperture; the subroutine comprising the steps of inputting radar data from a radar antenna; passing the radar signal through low noise amplifier to reduce impact of electronic noise from the radar system; down converting the signal with a mixer to obtain a lower frequency; filtering out harmonics from the higher frequency range; sampling the radar data using an analog to digital converter at least at Nyquist down range frequency; based upon the IF of the radar; determining a scene center (center of SAR imagery) for the purpose of motion compensation; performing a two stage averaging scheme of the received signals with a variable window function; determining a window function based upon the velocity and acceleration of the platform and scene center; the window function comprising a first stage window; coherently averaging N pulses together to create an average pulse; performing an inverse Fourier transform; compensating to the scene center by multiplying by a complex exponential based upon both the GPS and inertial navigational system; summing the average pulses using low pass filter; the software programming operating to repeat the step of building up an average pulse a first predetermined number of times for a time period that is less than the Nyquist sample time interval; the software programming operating to repeat the step of building an average pulse for a predetermined number of times to generate a second predetermined number of average pulses; the software programming operating to perform a two dimensional inverse Fourier transform to obtain SAR image; outputting the SAR image on a display screen; and a display for displaying the outputted SAR image.
Owner:US SEC THE ARMY THE

Method and apparatus for waypoint services navigational system

A Waypoint Services Navigational System (WSNS) is disclosed comprising a mobile unit connected to a server and to a database by the Internet. The WSNS uses omnipresent digital cellular links or any other form of radio frequency communications for transmission of information by a registered services provider to a traveler with a WSNS mobile unit. Using WSNS, the registered service provider announces its presence along with specific services/products to a traveler with a WSNS mobile unit within a predefined geographic radius. This information may be viewed via a conventional mobile computer, a personal digital assistant screen, or through a Global Positioning System (GPS) mapping longitude/latitude device. The WSNS mobile unit may be portable or mounted in a vehicle in a convenient location. Specific directions to a selected services provider are provided based upon the proximity positioning information at that moment in-time when the information is requested. Advertising specials, competitive services/products, entertainment, or emergency services may all be broadcast, and the user may choose from menus for the nature of services desired. Information may be provided regarding “upcoming” service providers through a combination of user geographical location, user directional data, and overlay maps showing registered businesses. Products or services may be ordered through a WSNS online order system for placing credit-or account backed purchases using the WSNS combination of locational information and business registration. WSNS service may also be provided through conventional internet-only communications, downloadable into a GPS-attached mobile computer to alleviate the need for a cellular link to the car.
Owner:SYBASE INC

Computationally efficent radar processing method and sytem for SAR and gmti on a slow moving platform

A method and system for processing radar data obtained from a platform which is subjected to non-uniform movement, the distance the platform travels during the formation of an image comprising an aperture; the system comprising software programming for performing a subroutine for building up an average pulse representing a single point on the aperture; the subroutine comprising the steps of inputting radar data from a radar antenna; passing the radar signal through low noise amplifier to reduce impact of electronic noise from the radar system; down converting the signal with a mixer to obtain a lower frequency; filtering out harmonics from the higher frequency range; sampling the radar data using an analog to digital converter at least at Nyquist down range frequency; based upon the IF of the radar; determining a scene center (center of SAR imagery) for the purpose of motion compensation; performing a two stage averaging scheme of the received signals with a variable window function; determining a window function based upon the velocity and acceleration of the platform and scene center; the window function comprising a first stage window; coherently averaging N pulses together to create an average pulse; performing an inverse Fourier transform; compensating to the scene center by multiplying by a complex exponential based upon both the GPS and inertial navigational system; summing the average pulses using low pass filter; the software programming operating to repeat the step of building up an average pulse a first predetermined number of times for a time period that is less than the Nyquist sample time interval; the software programming operating to repeat the step of building an average pulse for a predetermined number of times to generate a second predetermined number of average pulses; the software programming operating to perform a two dimensional inverse Fourier transform to obtain SAR image; outputting the SAR image on a display screen; and a display for displaying the outputted SAR image.
Owner:UNITED STATES OF AMERICA THE AS REPRESENTED BY THE SEC OF THE ARMY

Flight management system and method for providing navigational reference to emergency landing locations

An aviation navigational system and method for predicting glide range for an aircraft for specific airports and other potential emergency landing locations in proximity to the aircraft. Information is presented to the pilot by complementing a conventional moving map display with symbols centered on each landing location. GPS altitude, airport elevation, and the aircraft's glide ratio are factored into an equation to determine glide range for each airport within proximity to the aircraft. A circular symbol representing the glide range boundary is displayed around each airport. Each circular symbol represents a sectional view of an imaginary inverted cone, having the apex thereof centered on a given landing location. The size and shape of the cone is based on the gliding performance of the aircraft and the altitude differential between the aircraft and the target landing location. As the altitude differential increases the radius of the circle increases. Conversely as the altitude differential decreases, the radius of the circle decreases. As long as the aircraft is anywhere within any one of the three-dimensional inverted cones displayed, as represented by one or more circles on a two dimensional display, it can safely glide to the landing location. This display concept is selectively referred to herein as “cones of safety.”
Owner:CONTROL VISION CORP

Flight management system and method for providing navigational reference to emergency landing locations

An aviation navigational system and method for predicting glide range for an aircraft for specific airports and other potential emergency landing locations in proximity to the aircraft. Information is presented to the pilot by complementing a conventional moving map display with symbols centered on each landing location. GPS altitude, airport elevation, and the aircraft's glide ratio are factored into an equation to determine glide range for each airport within proximity to the aircraft. A circular symbol representing the glide range boundary is displayed around each airport. Each circular symbol represents a sectional view of an imaginary inverted cone, having the apex thereof centered on a given landing location. The size and shape of the cone is based on the gliding performance of the aircraft and the altitude differential between the aircraft and the target landing location. As the altitude differential increases the radius of the circle increases. Conversely as the altitude differential decreases, the radius of the circle decreases. As long as the aircraft is anywhere within any one of the three-dimensional inverted cones displayed, as represented by one or more circles on a two dimensional display, it can safely glide to the landing location. This display concept is selectively referred to herein as “cones of safety.”
Owner:CONTROL VISION CORP

Multifunctional collimator indicator

The present invention relates to indication systems providing augmented visual support for the operator of a motor vehicle, vessel or an aircraft. The indication system is positioned in the location of a traditional vehicular gauge dashboard. The indication system consists of an image formulator and an optical collimator system with two visual channels. Lower channel is used for direct visual tracking of all virtual gauge readings while the upper channel is used to track updates “on the windshield” of a vehicle with the background of the surrounding environment. The lower channel displays virtual collimator imaging of the traditional analog or digital gauges as well as navigational system data. The upper channel is reflected onto the exterior background of the windshield and displays collimator imaged critical data that is required for the safe operation of a vehicle. To provide the switching functionality between the two channels, the indication system utilizes a lightproof partition. The side of the partition facing the image formulator is designed as a flat reflective mirror. In order to engage the lower channel, the partition is placed away from the optical systems for the lower channel. To provide viewing of the upper channel, the partition is positioned along the optical axis of the upper collimator lens at a given angle. To provide the function of automatic switching between the channels, the multifunctional collimator indicator is equipped with an eye position tracking system which tracks real-time position of the eye's pupil.
Owner:LVOVSKIY MATVEY +3

Zero base line self-closed-loop satellite and ground time synchronizing method in pseudo global positioning system

The invention discloses a zero base line self-closed-loop satellite and ground time synchronizing method in a pseudo global positioning system. The method comprises the following steps: firstly, a pseudo satellite navigational signal is generated by a pseudo satellite signal generator with trigger pulse serving as time reference and is sent to a closed-loop navigational receiver under the condition of a zero base line; secondly, the closed-loop navigational receiver simultaneously receives a pseudo satellite signal and a space satellite navigational signal and satellite and ground synchronizing clock correction is calculated according to a pseudo satellite distance measurement value and a navigational satellite distance measurement value which are output by the receiver; thirdly, the satellite and ground synchronizing clock correction is processed, a rough clock correction control word and a precise clock correction parameter are obtained, the rough clock correction control word is sent to the signal generator, and satellite and ground rough synchronization is achieved; and fourthly, the precise clock correction parameter is written in a pseudo satellite telegraph text so that satellite and ground precise synchronization is achieved. The zero base line self-closed-loop satellite and ground time synchronizing method in the pseudo global positioning system can achieve high accuracy time synchronization of the pseudo global positioning system and a space satellite navigational system and has the advantages of being low in cost, simple and practical.
Owner:NO 54 INST OF CHINA ELECTRONICS SCI & TECH GRP
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