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

Dead reckoning optoelectronic intelligent docking system

Patent 4834531 Issued on May 30, 1989. Estimated Expiration Date: Icon_subject May 30, 2006. 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

3224709

3285533

3666367

3781111

3796492

3897150

3917196

Single plane corner reflector guidance system
Patent #: 4003659
Issued on: 01/18/1977
Inventor: Conard ,   et al.

System for detecting the presence of a possibly moving object
Patent #: 4026654
Issued on: 05/31/1977
Inventor: Beaurain

Focussed doppler radar
Patent #: 4167329
Issued on: 09/11/1979
Inventor: Jelalian ,   et al.

More ...

Inventor

Assignee

Application

No. 06/793292 filed on 10/31/1985

US Classes:

356/5.08, Including specific counter type timing of returns244/172.4, Rendezvous or docking348/140, Distance by apparent target size (e.g., stadia, etc.)356/139.03Relative attitude indication along 3 axes with photodetection

Examiners

Primary: Buczinski, Stephen C.
Assistant: Wallace, Linda J.

Attorney, Agent or Firm

International Classes

G05D 1/12 (20060101)
B64G 1/64 (20060101)
G01S 17/00 (20060101)
G01S 17/87 (20060101)

Abstract

An intelligent, optoelectronic docking system for use in manned or unmanned spacecraft for automatically docking with a target spacecraft. The system is a multifaceted, active sensor using a controlling microprocessor to integrate the operation of independently triggerable laser sources for target illumination and optical receiver arrays for target detection. Returning signal waveforms are processed to sense the direction, range, and attitude of a target docking surface which may be equipped with passive optical aids to enhance the reflective signature. The docking system reconfigures its active sensor elements as the target range closes by sequentially employing three laser transceiver arrangements. As a result, the system effectively tracks a target from a range of several hundred meters down to a range of only a few centimeters. The system microprocessor operates on data received from each sensor arrangement to generate the information necessary to guide a host spacecraft safely through hard docking maneuvers. Wide field coverage is achieved without moving parts by electronic selection of independently directed laser beams.

PatentsPlus Images
Enhanced PDF formats
loading...
PatentsPlus: add to cart
PatentsPlus: add to cartSearch-enhanced full patent PDF image
$9.95more info
PatentsPlus: add to cart
PatentsPlus: add to cartIntelligent turbocharged patent PDFs with marked up images
$16.95more info
 
Sign InRegister
Username  
Password   
forgot password?