公开(公告)号：CA2114551A1

公开(公告)日：1993-03-18

申请号：CA2114551

申请日：1992-07-31

Applicant: UNITED TECHNOLOGIES CORP

Inventor： GOLD PHILLIP J ,  FAULL WALTER R

IPC: B64C13/18 ,  G05D1/08

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 low speed 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：ES2110517T3

公开(公告)日：1998-02-16

申请号：ES92918348

申请日：1992-07-31

Applicant: UNITED TECHNOLOGIES CORP

Inventor： GOLD PHILLIP J ,  FAULL WALTER R

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 low speed 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：CA2114551C

公开(公告)日：1998-05-05

申请号：CA2114551

申请日：1992-07-31

Applicant: UNITED TECHNOLOGIES CORP

Inventor： GOLD PHILLIP J ,  FAULL WALTER R

IPC: B64C13/18 ,  G05D1/08

Abstract: A helicopter flight control system (21) includes a model following control syste m architecture which automatically provides a coordinating yaw command signal to the helicopter tail rotor to coordinate hel icopter flight during a low speed banked turn. The control system processes information from a variety of helicopter sensors (3 1) 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：AU657359B2

公开(公告)日：1995-03-09

申请号：AU2474492

申请日：1992-07-31

Applicant: UNITED TECHNOLOGIES CORP

Inventor： GOLD PHILLIP J ,  FAULL WALTER R

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 low speed 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.