Scanning horizon sensors using an inner and an outer radiation senstive detector

• US 5,095,199 A
• Filed: 09/11/1989
• Issued: 03/10/1992
• Est. Priority Date: 09/11/1989
• Status: Expired due to Fees

• Current Assignee: Ithaco Incorporated Clinton Street Ithaca NY 14851, Space Sciences Corp.
• Original Assignee: Ithaco Space Systems, Inc. (Raytheon Technologies Corporation d/b/a RTX), Space Sonics Incorporated
• Inventors: Selby, Vaughn, Fallon, James J.
• Primary Examiner(s): Nelms, David C.
• Assistant Examiner(s): ALLEN, STEPHONE B
• Application Number:
  US07/405,442
• Time in Patent Office: 911 Days
• Field of Search: 250/211 R, 250/211 J, 250/203.1, 250/203.4, 250/203.6, 250/347, 250/352, 250/206.1, 250/206.2
• US Class Current: 250/206.2
• CPC Class Codes: G01S 3/781 Details
• CPC Class Codes: G01S 3/7868 using horizon sensors

Abstract

Method and apparatus for accurately determining the horizon position of a celestial body is disclosed in the form of inner and outer detector portions arranged generally-concentrically relative to an optical axis. Difference-determining electrical circuitry determines a difference between the outputs of the two detectors.

Claims

1. A scanning horizon sensor which comprises, in combination:

optical means, and a detector assembly, said optical means having an optical axis and being operative to direct received radiation onto said detector assembly, wherein said detector assembly comprises an inner radiation-sensitive detector element and an outer radiation-sensitive detector element surrounding and spaced from said inner element relative to said optical axis, and difference-determining means connected to said detector elements for deriving a signal commensurate with a difference between the radiation received by said inner detector element and the radiation received by said outer detector element.

2. A sensor according to claim 1 wherein said inner detector element comprises a circular element centered on said optical axis, and said outer detector element comprises an annular element concentrically spaced on said optical axis relative to said inner detector element.

3. A sensor according to claim 1 wherein said inner and outer detector elements comprise first and second electrode coatings carried on a common substrate.

4. A sensor according to claim 1 wherein said difference-determining means comprises respective impedance-conversion means connected to said inner and outer detector elements, and differential amplifier means connected to the impedance-conversion means.

5. A sensor according to claim 1 wherein the radiation-sensitive areas of said inner and outer detector elements, and the gains with which signals from said detector elements are respectively connected to said differencing means are so selected that the signal produced by differencing means is substantially zero both (1) when both of said detector elements are receiving no substantial radiation and (2) when the entire areas of both of said detector elements are receiving a given amount of radiation.

6. A sensor according to claim 3 wherein the effective areas of said first and second electrode coatings are substantially equal.

7. A sensor according to claim 3 having a groove provided in said substrate between said first and second electrode coatings to decrease thermal conductance from one of said electrode coatings to the other of said electrode coatings.

8. The method of detecting a horizon crossing which comprises the steps of:

moving an optical field-of-view across a detector assembly having an inner radiation-sensitive detector element and an outer radiation-sensitive detector element surrounding and spaced from said inner element relative to the optical axis of said optical field-of-view; and

deriving a signal commensurate with a difference between the radiation being received by said inner detector element and the radiation received by said outer detector element.

9. The method of claim 8 wherein said step of moving said field-of-view comprises moving said field-of-view across inner and outer radiation-sensitive elements mounted on a substrate in substantially the same plane.