This patent is on a laser attitude detection and guidance system which uses a number of ground 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.
Single Plane Corner Reflector Guidance System
1974
5 pages
Report
Keine Angabe
Englisch
Corner Reflector simulation results
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