Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1976-06-17
1980-03-04
Engle, Samuel W.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
74 546, 74 56E, F42B 1328, F41G 710, G01C 1953, G01C 1928
Patent
active
041913469
ABSTRACT:
A body is provided which consists of several discrete portions at least on one portion of which is spin stabilized. Mechanism is carried by the body for generating a signal having a frequency proportional to the spin frequency of the spin stabilized portion of the body, together with means responsive to the signal for precessing at least a portion of the body. The signal for precessing the portion of the body can apply cyclically phased impulses correlative to the spin of the body to precess the body.
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Engle Samuel W.
Finch Walter G.
Finch Walter G.
Webb Thomas H.
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