Single plane corner reflector guidance system

Details Single plane corner reflector guidance system Single plane corner reflector guidance system

1974-11-15

1977-01-18

Wilbur, Maynard R.

Optics: measuring and testing

Angle measuring or angular axial alignment

With photodetection remote from measured angle

356 5, 244 311, G01B 1126, F41G 700

Patent

active

040036596

ABSTRACT:
A laser attitude detection and guidance system which uses a number of gro base laser transmitter/detector stations and at least two retroreflecting arrays on the missile to track and determine attitude correction signals to be sent for correcting the attitude of the missile relative to a predetermined trajectory.

REFERENCES:
patent: 3098933 (1963-07-01), Barasch
patent: 3478212 (1969-11-01), Turck
patent: 3574466 (1971-04-01), Peters
patent: 3698811 (1972-10-01), Weil
patent: 3731103 (1973-05-01), O'Meara
patent: 3746288 (1973-07-01), Schoneborn
patent: 3796396 (1974-03-01), Crovella
patent: 3866229 (1975-02-01), Hammack

Affiliated with

Also associated with

Rating

Single plane corner reflector guidance system does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Single plane corner reflector guidance system, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Single plane corner reflector guidance system will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-69281