Thrust vector control for large deflection angles

Details Thrust vector control for large deflection angles Thrust vector control for large deflection angles

1981-03-06

1983-05-24

Bentley, Stephen C.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

23926527, F42B 1518

Patent

active

043846904

ABSTRACT:
A missile thrust vector control system using fixed valves and nozzles in n numbers, as 4 or 8, mounted so that the thrust vectors operate at preselected angles to the frame and are pulse modulated in certain combinations to produce thrust vectors the sums of which provide desired deflections in pitch, yaw, and roll, without altering axial propulsion thrust.

REFERENCES:
patent: 2965334 (1960-12-01), McCullough, Jr. et al.
patent: 3115887 (1963-12-01), McCorkle
patent: 3255971 (1966-06-01), Widell
patent: 3292865 (1966-12-01), Short et al.
patent: 3478965 (1969-11-01), Llewellyn
patent: 3502288 (1970-03-01), Pavlin et al.
patent: 3599899 (1971-08-01), McCullough
patent: 3726496 (1973-04-01), Leonard
patent: 3944172 (1976-03-01), Becker
patent: 4017040 (1977-04-01), Dillinger et al.

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