Projectile guidance
AssigneeSociete Europeene de Propulsion
InventorJean Tubeuf
Life of this patent
Estimating the term…
Abstract
A projectile guidance system employs entry and exit ports for the ambient fluid medium with fluidic circuits interconnecting various of the entry and exit ports so that asymmetry of the flow through the ports will be induced merely by regulating the flow in any given fluidic circuit. Control means signalling trajectory correction instructions is effective to regulate the flow to orient the asymmetry such as to induce the desired yawing torque on the projectile. Where the projectile is spinning the regulating effect will be switched between the ports and will be effective at a station 90.degree. displaced about the projectile longitudinal axis of symmetry from the direction in which yawing movement is desired.
Claims5
In combination with a spinning projectile having no external aerodynamic control surfaces the improvement of a projectile control system which comprises:
- a. means for signalling trajectory correction instructions;
- b. means defining at least one entry port for the ambient fluid medium;
- c. means defining at least one exit port for said ambient fluid medium and means connecting said exit and entry ports;
- d. said entry and exit ports being offset relative to the longitudinal axis of symmetry of said projectile;
- e. said connecting means comprising an assembly of fluidic circuits;
- and
- f. magnetostrictive means responsive to said trajectory instructions signalled by a control means for regulating the flow of fluid through at least one of said fluidic circuits for controlling flow through at least one of said entry and exit ports.
A projectile comprising control means for signalling trajectory correction instructions and guiding means responsive to said control means, said guiding means comprising a plurality of entry ports for the ambient fluid medium arranged around periphery of the body of the projectile, at least an exit port for the ambient fluid medium, an assembly of fluidic circuits located within the body of the projectile and interconnecting said entry and exits ports, and means for regulating the flow of fluid through said fluidic circuits in order to selectively control the flow of fluid passing through at least one of said entry and exit ports which is offset relative to the longitudinal axis of symmetry of the projectile, said regulating means comprising magnetostrictive actuator means responsive to said control means.
Dependencies are inferred from the claim text.