公开(公告)号：AU655845B2

公开(公告)日：1995-01-12

申请号：AU2598192

申请日：1992-08-21

Applicant: UNITED TECHNOLOGIES CORP

Inventor： FOGLER DONALD L JR ,  RICHARD JAMES L ,  GOLD PHILLIP J ,  GLUSMAN STEVEN I

IPC: A61K31/40 ,  A61K31/4025 ,  A61K31/435 ,  A61P1/00 ,  A61P9/00 ,  A61P9/10 ,  A61P9/12 ,  A61P11/00 ,  A61P11/08 ,  A61P13/02 ,  A61P15/00 ,  B64C13/18 ,  B64C27/12 ,  C07D405/04 ,  G05D1/00 ,  G05D1/06 ,  G05D1/08

Abstract: A helicopter flight control system (21) includes a model following control system architecture which operates in a velocity command mode at low ground speeds. The control system processes information from a variety of helicopter sensors (31) in order to provide a command signal to the main rotor (11) of the helicopter which results in a ground speed which is proportional to the input provided via a sidearm controller (29).

公开(公告)号：CA2116565A1

公开(公告)日：1993-03-18

申请号：CA2116565

申请日：1992-08-21

Applicant: UNITED TECHNOLOGIES CORP

Inventor： FOGLER DONALD L JR ,  RICHARD JAMES L ,  GOLD PHILLIP J ,  GLUSMAN STEVEN I

IPC: A61K31/40 ,  A61K31/4025 ,  A61K31/435 ,  A61P1/00 ,  A61P9/00 ,  A61P9/10 ,  A61P9/12 ,  A61P11/00 ,  A61P11/08 ,  A61P13/02 ,  A61P15/00 ,  B64C13/18 ,  B64C27/12 ,  C07D405/04 ,  G05D1/00 ,  G05D1/06 ,  G05D1/08

Abstract: A helicopter flight control system (21) includes a model following control system architecture which operates in a velocity command mode at low ground speeds. The control system processes information from a variety of helicopter sensors (31) in order to provide a command signal to the main rotor (11) of the helicopter which results in a ground speed which is proportional to the input provided via a sidearm controller (29).

公开(公告)号：ES2078753T3

公开(公告)日：1995-12-16

申请号：ES92920165

申请日：1992-08-21

Applicant: UNITED TECHNOLOGIES CORP

Inventor： FOGLER DONALD L JR ,  RICHARD JAMES L ,  GOLD PHILLIP J ,  GLUSMAN STEVEN I

IPC: A61K31/40 ,  A61K31/4025 ,  A61K31/435 ,  A61P1/00 ,  A61P9/00 ,  A61P9/10 ,  A61P9/12 ,  A61P11/00 ,  A61P11/08 ,  A61P13/02 ,  A61P15/00 ,  B64C13/18 ,  B64C27/12 ,  C07D405/04 ,  G05D1/00 ,  G05D1/06 ,  G05D1/08

Abstract: A helicopter flight control system (21) includes a model following control system architecture which operates in a velocity command mode at low ground speeds. The control system processes information from a variety of helicopter sensors (31) in order to provide a command signal to the main rotor (11) of the helicopter which results in a ground speed which is proportional to the input provided via a sidearm controller (29).