Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1989-05-03
1990-11-06
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
244 314, F41G 728
Patent
active
049679813
ABSTRACT:
System for determining the angular spin position of an object (1) spinning about an axis situated within certain limits near the surface (2) of a celestial body. The system is provided with means (4, 5, 6) for generating at least one carrier wave (7, 8) reaching as far as the surroundings of the object (1) and up to and interfering with the surface (2). The system is further provided with directional receiving antenna means (16) fitted to the object (1) and a receiving system (19) linked thereto for determining the angular spin position of the object (1) with respect to the surface (2) on the basis of the angular spin position of the object (1) with respect to the polarization direction of the carrier wave (7, 8).
REFERENCES:
patent: 2995749 (1961-08-01), Robinson, Jr.
patent: 4219170 (1980-08-01), Esker
patent: 4328938 (1982-05-01), Reisman et al.
patent: 4750689 (1988-06-01), Yff
Hollandse Signaalapparaten B.V.
Jordan Charles T.
Kraus Robert J.
Lieberman Rochelle
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