Accession Number : ADD001521

Title :   Combined Vertical and Lateral Identical Location of Accelerometer and Force System.

Descriptive Note : Patent,

Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON D C

Personal Author(s) : Wykes,John H ; Mori,Alva S ; Hoge,Harvey J

Report Date : 02 Sep 1975

Pagination or Media Count : 7

Abstract : The patent relates to a structural mode control system having sensing elements to operate control force application devices, such as aerodynamic control vanes. The sensing elements are located at the control force application point.

Descriptors :   *Aerodynamic control surfaces, *Control systems, *Patents, Supersonic flight, Bending, Control, Accelerometers

Subject Categories : Aerodynamics
      Aircraft

Distribution Statement : APPROVED FOR PUBLIC RELEASE