U.S. Patent Specifications

Abstract

In combination with dirigible craft provided with means for directing the same, power mechanism for actuating said directing means and means sensitive to turn of the craft, means for integrating the extent of turn and a separate device sensitive to acceleration, all connected to conjonitly control operation of said power mechanism.

Citation

(1943), "U.S. Patent Specifications", Aircraft Engineering and Aerospace Technology, Vol. 15 No. 3, pp. 91-92. https://doi.org/10.1108/eb031002