Single plane corner reflector guidance system
US4003659A · kind A · utility
21Cited by
8References
4Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Nov 15, 1974 |
| Grant date | Jan 18, 1977 |
| Priority date | — |
| Expiry date | Nov 15, 1994 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF41G7/30
- WIPO fieldOther special machines
- WIPO sectorMechanical engineering
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.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.