Method, Device and Computer Program for Determining the Position of a Satellite Using a Star Tracker

    公开(公告)号:US20240425209A1

    公开(公告)日:2024-12-26

    申请号:US18703621

    申请日:2022-10-26

    Inventor: Uwe Schmidt

    Abstract: A method for determining the position of a satellite rotating about an axis of rotation using at least a star tracker which is aligned along an optical axis with a recorded light object field, the axis of rotation and the optical axis being at a fixed angle relative to one another and a light sensor having a sensor surface which is perpendicular to the optical axis and contains a sensor coordinate system having an arrangement of light-sensitive pixels in rows being provided. To achieve improved position control of the satellite, image data recorded in the individual rows of the light sensor are recorded row by row and sequentially, the image data for each row are convoluted with a predefined number of pixels over a predefined time interval using a boxcar operator, a light maximum is identified using the boxcar operator, the light maximum is assigned to a location of a light object on the basis of a position of the row and within the row in the sensor coordinate system, and an object list containing light object coordinates, the light maximum and a measurement time is identified from a plurality of light objects using an over the entire sensor coordinate system.

    Vertical Navigation system
    7.
    发明申请

    公开(公告)号:US20230098784A1

    公开(公告)日:2023-03-30

    申请号:US18075142

    申请日:2022-12-05

    Abstract: Aspects of the disclosure are directed to acquiring aligned geographic coordinates of a vertical position. In one aspect, a vertical navigation system includes a light source to generate a source beam; a beam splitter to generate a first and a second source references derived from the source beam; a hollow retroreflector to produce a first and a second vertical references derived from the first and the second source references; an attitude sensor to capture a plurality of reference stars and to measure a first set of angles for the first vertical reference and a second set of angles for the second vertical reference, the first set of angles and the second set of angles are relative to the plurality of reference stars; and a processor to produce the aligned geographical coordinates using the first set of angles, the second set of angles, a gravity vector measurement and a time signal.

    POSITION SPACE IDENTICATION METHOD, POSITION SPACE IDENTIFIER IMPARTING DEVICE, AND COMPUTER PROGRAM

    公开(公告)号:US20220236062A1

    公开(公告)日:2022-07-28

    申请号:US17629203

    申请日:2020-07-22

    Inventor: Masafumi TAKEDA

    Abstract: The present invention provides a method for imparting unique identifiers that do not overlap each other to individual position spaces in the case of latitude and longitude information or even in the case of height information also included in addition thereto. A longitude line passing through the coordinate origin is divided by the length of one side of a unit grid, and a latitude value inside unit grids is calculated. An accumulated error is calculated in a case where latitude values inside the unit grids are accumulated for one round in a longitude line direction of a celestial body, and an error per unit grid is calculated based on the calculated accumulated error. The number of unit grids included in one block in the longitude line direction is specified so that a reference error per block is equal to or smaller than one thousandth of the accumulated error, and thus a reference latitude is set. A reference longitude is set by the same calculation process for each latitude line that is determined based on the set reference latitude, reference points are specified sequentially from the coordinate origin based on the set reference latitude and reference longitude, and a unique identifier is imparted to each unit grid located in a block with the reference points set as its vertices.

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