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US4618259A Expired / Lapsed US ⏱️ 0.0 years remaining

Star and sun sensor for attitude and position control

Assignee: Airbus Defence and Space GmbH
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Filing: 1985-04-01
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Granted: 1986-10-21
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Expires: 2005-04-01
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Abstract

Abstract A combined sun and star sensing system for attitude and position control of a space vehicle, includes a star image sensor having a first objective and a first detector array arranged in the focal plane, the objective being constructed for a well defined aberration so as to convert a point like object into a defined spot or area having a diameter larger than the diameter of an element of the detector array; the sun sensor has a regular objective and a second detector array is arranged in the image plane of that objective sun sensor; the two detector arrays have similar and a similar number of detector elements, and are alternately connected to a single evaluating electronic.

Inventors

  • 👤 Reinhard Czichy
  • 👤 Wilhelm Goeschel

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-02 20:45
CPC Classifications
G; G01; G01S; G01S5/00; G01S5/16; G01S5/163; G01S3/00; G01S3/78; G01S3/782; G01S3/785; G01S3/786

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 164 words
A combined sun and star sensing system for attitude and position control of a space vehicle, comprising: a star image sensor, including a first objective lens or lens system having a focal and image plane, there being a first detector array arranged in said image plane; said objective or objective lens system being constructed for a well defined aberration so as to convert a point like object into a defined spot or area having a diameter larger than the diameter of an element of said first detector array; a sun sensor including a second objective lens or lens system having an image and focal plane, there being a second detector array being arranged in the image plane of said second objective of the sun sensor; said first and second detector arrays having similar and a similar number of detector elements; a single evaluating electronic for detector array images; and switching means for selectively connecting said first and said detector array to said evaluating electronic.
Claim 2
Dependent Claim 164 words
A combined sun and star sensing system for attitude and position control of a space vehicle, comprising: a star image sensor, including a first objective lens or lens system having a focal and image plane, there being a first detector array arranged in said image plane; said objective or objective lens system being constructed for a well defined aberration so as to convert a point like object into a defined spot or area having a diameter larger than the diameter of an element of said first detector array; a sun sensor including a second objective lens or lens system having an image and focal plane, there being a second detector array being arranged in the image plane of said second objective of the sun sensor; said first and second detector arrays having similar and a similar number of detector elements; a single evaluating electronic for detector array images; and switching means for selectively connecting said first and said detector array to said evaluating electronic.
Claim 3
Dependent Claim 35 words
A combination as in claim 1, wherein said first objective lens or lens system or the star sensor provides for a correction of the chromatic aberration through a spectral range from 0.3 to 1.2 micrometers.
Claim 4
Dependent Claim 20 words
A combination as in claim 1, wherein said first objective lens or lens system provides a spherical aberration or apodisation.
Claim 5
Dependent Claim 27 words
A combination as in claim 1, wherein said evaluating electronics is constructed to determine the center of any image spot, independently from a source for the spot.

References Cited (Backward Citations)

US3931515A Cited
US3744913A Cited
US4225781A Cited
US4367403A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1989-10-20 1990-04-21 1990-10-21 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1993-10-20 1994-04-21 1994-10-21 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1997-10-20 1998-04-21 1998-10-21 $7700.00 Window Closed / Lapsed

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