Method and sensor for capturing rate and position and stabilization of a satellite using at least one focal plane
First Claim
1. A method for determining direction and rate of rotation of a satellite about first, second, and third mutually orthogonal body axes fixed relative to the satellite and for determining orientation of the satellite relative to earth, comprising:
- mounting a dual field-of-view optical sensor on the satellite with an optical axis of the sensor in a predetermined orientation with respect to the body axes, the sensor having at least one focal plane array comprising a plurality of pixels arranged as a grid;
directing radiant energy from a first field of view of the sensor onto a first annular region of the at least one focal plane array, the first field of view spanning 360°
in azimuth angle about the optical axis and a range of elevation angles including 90°
in elevation angle relative to the optical axis;
directing radiant energy from a second field of view of the sensor onto a second annular region of the at least one focal plane array, the second field of view spanning 360°
in azimuth angle about the optical axis and a range of elevation angles non-perpendicular to the optical axis;
determining a relative location of a subtense of a limb of the earth on the first annular region of the at least one focal plane array at each of a plurality of successive times, and determining direction and rate of rotation of the satellite about the body axes based on changes in the relative location of the earth limb subtense on the first annular region; and
determining a relative location of the earth limb subtense on the second annular region of the at least one focal plane array, and determining orientation angles between the body axes and a nadir vector to the earth based on the relative location of the earth limb subtense on the second annular region.
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Accused Products
Abstract
An optical sensor includes dual fields of view including a panoramic field of view spanning 360° in azimuth angle in a direction perpendicular to an axis of the sensor, and a limb-looking field of view non-perpendicular to the axis for viewing the limb of the earth. Both fields of view are imaged onto annular regions of one of more focal plane arrays comprising pixels arranged in a rectangular array of rows and columns. The sensor is used in a method for capturing rate and direction of rotation of a satellite about its axes and for detecting orientation of the satellite about two of its axes. Rate and direction are determined by finding the center of the earth relative to axes of the focal plane array based on the image of the earth limb from the panoramic field of view, and comparing the earth center location at a series of sequential times. The rate and position information are used for stabilizing an initially tumbling satellite after tip-off. Once the satellite is stabilized, its orientation is detected by finding the earth center location on the focal plane array based on the earth limb image from the limb-looking optics of the sensor. In one embodiment of the invention, both fields of view are imaged onto concentric inner and outer ring-shaped regions of the same focal plane array.
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Citations
31 Claims
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1. A method for determining direction and rate of rotation of a satellite about first, second, and third mutually orthogonal body axes fixed relative to the satellite and for determining orientation of the satellite relative to earth, comprising:
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mounting a dual field-of-view optical sensor on the satellite with an optical axis of the sensor in a predetermined orientation with respect to the body axes, the sensor having at least one focal plane array comprising a plurality of pixels arranged as a grid;
directing radiant energy from a first field of view of the sensor onto a first annular region of the at least one focal plane array, the first field of view spanning 360°
in azimuth angle about the optical axis and a range of elevation angles including 90°
in elevation angle relative to the optical axis;
directing radiant energy from a second field of view of the sensor onto a second annular region of the at least one focal plane array, the second field of view spanning 360°
in azimuth angle about the optical axis and a range of elevation angles non-perpendicular to the optical axis;
determining a relative location of a subtense of a limb of the earth on the first annular region of the at least one focal plane array at each of a plurality of successive times, and determining direction and rate of rotation of the satellite about the body axes based on changes in the relative location of the earth limb subtense on the first annular region; and
determining a relative location of the earth limb subtense on the second annular region of the at least one focal plane array, and determining orientation angles between the body axes and a nadir vector to the earth based on the relative location of the earth limb subtense on the second annular region. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14)
substantially reducing tumbling of the satellite by applying corrective thrusts to the satellite based on the rates and direction of rotation determined from the first field of view of the sensor; and
placing and stabilizing the satellite in a predetermined orientation relative to the nadir vector by applying stabilizing thrusts to the satellite based on the orientation angles determined from the second field of view of the sensor.
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3. The method of claim 1, wherein the first and second fields of view are directed respectively onto concentric first and second annular regions of the same focal plane array.
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4. The method of claim 3, wherein the first annular region comprises an inner ring and the second annular region comprises an outer ring lying radially outwardly of the inner ring.
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5. The method of claim 4, wherein the pixels of the focal plane array are arranged in a plurality of parallel rows and a plurality of parallel columns perpendicular to the rows, the relative location of the earth limb subtense being determined on each of the inner and outer rings by detecting transition pixels in each row and each column at which a transition between earth and space falls.
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6. The method of claim 1, wherein sensor electronics connected to the sensor capture signals from the at least one focal plane array by sampling the signals periodically to create a series of sequential frames, and wherein the location of the subtense of the earth limb on each of the annular regions is sampled at least three times for each frame.
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7. The method of claim 1, further comprising directing radiant energy from at least one of the fields of view onto more than one focal plane array.
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8. The method of claim 7, wherein a separate set of electronics is provided for each focal plane array to enable multiple signal paths for enhanced reliability.
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9. The method of claim 1, wherein the at least one focal plane array is operable to detect radiant energy in a wavelength band chosen so as to provide both day and night limb contrast and such that limb height changes caused by season and diurnal changes are minimized.
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10. The method of claim 9, wherein the wavelength band lies within a range from about 3.5 μ
- m to about 4.5 μ
m.
- m to about 4.5 μ
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11. The method of claim 1, wherein sensor electronics connected to the sensor capture signals from the at least one focal plane array by sampling the signals periodically at a defined sampling rate to create a series of sequential frames, and wherein the sampling rate is at least about 10 frames per second.
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12. The method of claim 1, wherein rotational orientations of the satellite about two of the body axes are determined from the second annular region of the at least one focal plane array, and further comprising determining a rotational orientation of the satellite about the third body axis by directional radio reception.
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13. The method of claim 1, wherein rotational orientations of the satellite about two of the body axes are determined from the second annular region of the at least one focal plane array, and further comprising determining a rotational orientation of the satellite about the third body axis by directional magnetic fields.
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14. The method of claim 1, wherein rotational orientations of the satellite about two of the body axes are determined from the second annular region of the at least one focal plane array, and further comprising determining a rotational orientation of the satellite about the third body axis by directional inertial rotation.
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15. A dual field-of-view optical sensor comprising:
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at least one focal plane array comprising a plurality of pixels arranged in a grid;
panoramic optics for capturing radiant energy from an annular panoramic field of view spanning 360°
in azimuth angle about an optical axis of the sensor and covering a range of elevation angles including 90°
in elevation angle relative to the optical axis, the panoramic optics re-directing and focusing the radiant energy from the panoramic field of view onto a first annular region of the at least one focal plane array; and
limb-looking optics for capturing radiant energy from an annular field of view spanning 360°
in azimuth angle about the optical axis and covering a range of elevation angles non-perpendicular to the optical axis such that at least a major circumferential portion of a limb of the earth is within the field of view of the limb-looking optics when the optical axis of the sensor points toward a centroid of the earth, the limb-looking optics re-directing and focusing the radiant energy onto a second annular region of the at least one focal plane array.- View Dependent Claims (16, 17, 18, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28)
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29. A method for determining direction and rate of rotation of a satellite about first, second, and third mutually orthogonal body axes fixed relative to the satellite, comprising:
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mounting an optical sensor on the satellite with an optical axis of the sensor in a predetermined orientation with respect to the body axes, the sensor having at least one focal plane array comprising a plurality of pixels arranged as a grid;
directing radiant energy from a panoramic field of view of the sensor onto an annular region of the at least one focal plane array, the panoramic field of view spanning 360°
in azimuth angle about the optical axis and a range of elevation angles including 90°
in elevation angle relative to the optical axis; and
determining a relative location of a subtense of a limb of the earth on the annular region of the at least one focal plane array at each of a plurality of successive times, and determining direction and rate of rotation of the satellite about the body axes based on changes in the relative location of the earth limb subtense on the annular region. - View Dependent Claims (30, 31)
substantially reducing tumbling of the satellite by applying corrective thrusts to the satellite based on the rates and direction of rotation determined from the panoramic field of view of the sensor.
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31. The method of claim 29, wherein the pixels of the focal plane array are arranged in a plurality of parallel rows and a plurality of parallel columns perpendicular to the rows, the relative location of the earth limb subtense being determined on the focal plane array by detecting transition pixels in each row and each column at which a transition between earth and space falls.
Specification