Aeronautics and astronautics – Spacecraft – Attitude control
Reexamination Certificate
2005-06-28
2005-06-28
Gregory, Bernarr E. (Department: 3662)
Aeronautics and astronautics
Spacecraft
Attitude control
C244S158700, C244S164000, C356S138000, C356S139030
Reexamination Certificate
active
06910660
ABSTRACT:
A guidance system includes a first laser device coupled to a mount, the first laser device adapted to generate a first laser signal having a first wavelength. A second laser device is also coupled to the mount and directed substantially parallel with the first laser device. The second laser device is adapted to generate a second laser signal having a second wavelength. A first photodiode is adapted to detect the first laser signal, retro-reflected from a first wavelength matched section of a reflector system, and the second laser, signal retro-reflected from a second wavelength matched section of the reflector system. The first photodiode is adapted to generate a first photodiode signal therefrom.
REFERENCES:
patent: 3224709 (1965-12-01), Blizard
patent: 3285533 (1966-11-01), Jernigan, Jr.
patent: 4026654 (1977-05-01), Beaurain
patent: 4834531 (1989-05-01), Ward
patent: 5493392 (1996-02-01), Blackmon et al.
Artz & Artz PC
Gregory Bernarr E.
The Boeing Company
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