U.S. patents available from 1976 to present.
U.S. patent applications available from 2005 to present.

Star sensor

Patent 4944587 Issued on July 31, 1990. Estimated Expiration Date: Icon_subject March 3, 2009. Estimated Expiration Date is calculated based on simple USPTO term provisions. It does not account for terminal disclaimers, term adjustments, failure to pay maintenance fees, or other factors which might affect the term of a patent.

Patent References

3263088

Error cancelling scanning optical angle measurement system
Patent #: 3992106
Issued on: 11/16/1976
Inventor: Auerbach

Analog apparatus for determining the attitude errors of a three-axis stabilized satellite
Patent #: 4084087
Issued on: 04/11/1978
Inventor: Mehwald

Stellar corrector
Patent #: 4306691
Issued on: 12/22/1981
Inventor: Boxenhorn ,   et al.

Artificial satellite attitude control system
Patent #: 4617634
Issued on: 10/14/1986
Inventor: Izumida ,   et al.

Star catalog navigation system
Patent #: 4621329
Issued on: 11/04/1986
Inventor: Jacob

Star sightings by satellite for image navigation Patent #: 4746976
Issued on: 05/24/1988
Inventor: Kamel ,   et al.

Inventor

Application

No. 318635 filed on 03/03/1989

US Classes:

356/139.01, Star/Sun/Satellite position indication with photodetection250/203.6, Airborne target, or spaceborne target other than the sun (e.g., star or missile)250/206.2, Detection of positional information in two or more planes (e.g., azimuth and elevation; hour angle and declination)701/222Using star tracker

Examiners

Primary: Jordan, Charles T.
Assistant: Wendtland, Richard W.

Attorney, Agent or Firm

International Class

B64G 001/36

Foreign Application Priority Data

1988-03-17 JP

Abstract

A star sensor compares predetermined star information stored in a memory and actual star information corresponding to star image signals from an imaging device. A processing device generates an attitude signal corresponding to the attitude of a base with respect to the star when the predetermined and the actual star information substantially coincide. A correcting device corrects the predetermined star information when the predetermined star information and the actual star information are not substantially the same.

Other References

  • IAF-84-375, "Autonomous GPS-INS-STAR Integrated Navigation System Concept for Maneuvering Spacecraft", T. Tanabe, M. Harigae and H. Koyama, Univ. of Tokyo, Oct. 7-13, 198
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