Star sensor for attitude detection of a spinning satellite

• US 4,740,681 A
• Filed: 03/19/1987
• Issued: 04/26/1988
• Est. Priority Date: 03/20/1986
• Status: Expired due to Fees

• Current Assignee: Kabushiki Kaisha Toshiba (Toshiba Corporation)
• Original Assignee: Kabushiki Kaisha Toshiba (Toshiba Corporation)
• Inventors: Tsuno, Katsuhiko
• Primary Examiner(s): Westin, Edward P.
• Assistant Examiner(s): Shami, Khaled
• Application Number:
  US07/028,089
• Time in Patent Office: 404 Days
• Field of Search: 250/203 R, 250/203 S, 250/578, 356/141, 356/152
• US Class Current: 250/206.2
• CPC Class Codes: G01S 3/7867 Star trackers navigation using star trackers G01C21/025
• CPC Class Codes: G01S 3/789 using rotating or oscillating beam systems, e.g. using mirrors, prisms

Abstract

A star sensor mounted in a satellite subjected to a spinning motion includes an optical system for obtaining an image of a fixed star, a CCD area sensor as an image pickup device arranged at a focal point of the optical system, a signal processing circuit for receiving an output from the CCD area sensor through a preamplifier, and a CCD driving circuit connected to the CCD area sensor. The CCD area sensor is an interline type CCD. The optical axis of the optical system is perpendicular to a spinning axis of the satellite. The horizontal scanning direction of the CCD area sensor coincides with the direction of the spinning axis. For this reason, the star image is moved on the light-receiving surface of the CCD area sensor along the vertical scanning direction with the spinning motion of the satellite. The CCD driving circuit causes the CCD area sensor to perform time-delay integration at a speed corresponding to the spinning speed of the satellite. After one-frame information obtained by the photoelectric transducer is transferred (frame shift) to the vertical transfer CCD arrays, only a one-horizontal line component is read out for a period between one frame shift and the next frame shift. Therefore, movement of the star image on the photoelectric transducer is synchronized with the transfer speed of the signal charge in the vertical transfer CCD arrays, and thus the signal charge of the star image can be integrated in the vertical transfer CCD arrays.

Claims

1. A star sensor mounted in a satellite which is subjected to a spinning motion, comprising:

an optical system for obtaining an image of a fixed star;

image pickup means for picking up the image of the fixed star, said image pickup means being provided with a photoelectric transducer having a large number of photoelectric transducer elements arranged in a matrix form, and a charge transfer section for sequentially scanning and reading out signal charges from said photoelectric transducer elements, a horizontal scanning direction of said image pickup means being adapted to coincide with a spinning axis of the satellite;

driving means for causing said image pickup means to perform time-delay integration at a speed in accordance with a spinning speed; and

means for calculating an azimuth and an elevation angle of the fixed star in response to signal output timings of said image pickup means within a spinning cycle.

2. A star sensor according to claim 1, in which said driving means repeats a cycle consisting of a frame shift step for shifting an output signal charge from said photoelectric transducer to said charge transfer section, a step for transferring, by one horizontal line, the signal charge shifted in said charge transfer section along a vertical scanning direction, and a read step for reading out a signal charge of one horizontal line, a repetition speed of the step for transferring the signal charge along the vertical scanning direction being equal to a moving speed of the image of the fixed star upon spinning of the satellite.

3. A star sensor according to claim 2, in which said image pickup means comprises an interline charge-coupled device.