Directional control system for artillery missiles

Details Directional control system for artillery missiles Directional control system for artillery missiles

1975-12-08

1977-05-17

Engle, Samuel W.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

2392651G, F42B 1330, F42B 1518, F41G 714, F41G 900

Patent

active

040237494

ABSTRACT:
Apparatus for controlling the powered flight phase of an artillery rocket a straight line as determined by a 2.degree. of freedom gyroscope with spin axis aligned along the missile axis. The flight path is made insensitive to crosswinds, launching transients, and missile thrust malalignments, without requiring lateral acceleration measurements.

REFERENCES:
patent: 2644296 (1953-07-01), Sanz et al.
patent: 2692475 (1954-10-01), Hull
patent: 2850977 (1958-09-01), Pollak
patent: 2969017 (1971-01-01), Kershner
patent: 3245352 (1966-04-01), Summers
patent: 3743184 (1973-07-01), Mancus
patent: 3946968 (1976-03-01), Stallard

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