公开(公告)号：ES2080512T3

公开(公告)日：1996-02-01

申请号：ES92917911

申请日：1992-07-31

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SKONIECZNY JOSEPH P ,  FOGLER DONALD L JR ,  GOLD PHILIPP J ,  KELLER JAMES F ,  DRYFOOS JAMES B

IPC: G05D1/08 ,  B64C13/18

Abstract: A helicopter flight control system (21) includes a model following control system architecture which automatically provides a coordinating yaw command signal to the helicopter tail rotor to coordinate helicopter flight during a banked turn. The control system processes information from a variety of helicopter sensors (31) in order to provide the coordinating yaw command signal on an output line (72) to the tail rotor (20) of the helicopter.

公开(公告)号：AU657165B2

公开(公告)日：1995-03-02

申请号：AU2462992

申请日：1992-07-31

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SKONIECZNY JOSEPH P ,  FOGLER DONALD L JR ,  GOLD PHILIPP J ,  KELLER JAMES F ,  DRYFOOS JAMES B

IPC: B64C13/18 ,  G05D1/08 ,  G05D1/00

Abstract: A helicopter flight control system (21) includes a model following control system architecture which automatically provides a coordinating yaw command signal to the helicopter tail rotor to coordinate helicopter flight during a banked turn. The control system processes information from a variety of helicopter sensors (31) in order to provide the coordinating yaw command signal on an output line (72) to the tail rotor (20) of the helicopter.