The interferometer homing system is for steering guided missiles toward a collision with a target. Two separated horn-type antennas are mounted upon the guided missile. The interferometer homing system produces a steering signal in which there appears no false information in the form of biases. The gyroscope compensation factor remains fixed throughout the flight of the missile.
Inter-Ferometer Homing System
1965
1 pages
Report
Keine Angabe
Englisch
Wiley | 2016
|Online Contents | 1997
Online Contents | 1994