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

Global positioning system synchronized active light autonomous docking system

Patent 5490075 Issued on February 6, 1996. Estimated Expiration Date: Icon_subject August 1, 2014. 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

Dead reckoning optoelectronic intelligent docking system
Patent #: 4834531
Issued on: 05/30/1989
Inventor: Ward

Standard remote manipulator system docking target augmentation for automated docking
Patent #: 5020876
Issued on: 06/04/1991
Inventor: Howard, et al.

Closed-loop autonomous docking system
Patent #: 5109345
Issued on: 04/28/1992
Inventor: Dabney, et al.

Optical range finder
Patent #: 5125736
Issued on: 06/30/1992
Inventor: Vaninetti, et al.

Spacecraft docking sensor system Patent #: 5334848
Issued on: 08/02/1994
Inventor: Grimm

Inventors

Assignee

Application

No. 283728 filed on 08/01/1994

US Classes:

701/226, Space orbits or paths701/23, Automatic route guidance vehicle701/82Antispin, traction control, or drive slip control

Examiners

Primary: Teska, Kevin J.
Assistant: Wieland, Susan

Attorney, Agent or Firm

International Class

B64G 001/64

Abstract

A Global Positioning System Synchronized Active Light Autonomous Docking System (GPSSALADS) for automatically docking a chase vehicle with a target vehicle comprising at least one active light emitting target which is operatively attached to the target vehicle. The target includes a three-dimensional array of concomitantly flashing lights which flash at a controlled common frequency. The GPSSALADS further comprises a visual tracking sensor operatively attached to the chase vehicle for detecting and tracking the target vehicle. Its performance is synchronized with the flash frequency of the lights by a synchronization means which is comprised of first and second internal clocks operatively connected to the active light target and visual tracking sensor, respectively, for providing timing control signals thereto, respectively. The synchronization means further includes first and second Global Positioning System receivers operatively connected to the first and second internal clocks, respectively, for repeatedly providing simultaneous synchronization pulses to the internal clocks, respectively. In addition, the GPSSALADS includes a docking process controller means which is operatively attached to the chase vehicle and is responsive to the visual tracking sensor for producing commands for the guidance and propulsion system of the chase vehicle.

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