Rotor setting system in conjunction with aerodynamic body contro

Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance

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F42B 15027, F41G 902

Patent

active

049270966

ABSTRACT:
A rotor setting system in conjunction with an aerodynamic-body control. The setting system is characterized by a rotor which comprises a console, a rotary drive for the rotor, setting members for the control of the aerodynamic body, especially rudders or spoilers, as well as a control unit for the rotor, and further including a control unit on the sides of the aerodynamic body, wherein the two control units cooperate with each other for adjusting the setting members.

REFERENCES:
patent: 3102437 (1963-09-01), Geyer
patent: 4210298 (1980-07-01), Liberman
patent: 4438893 (1984-03-01), Sands et al.

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