公开(公告)号：AU657001B2

公开(公告)日：1995-02-23

申请号：AU2506392

申请日：1992-08-26

Applicant: UNITED TECHNOLOGIES CORP

Inventor： WRIGHT STUART C ,  DRYFOOS JAMES B

IPC: B64C13/18 ,  B64C13/50 ,  G05D1/08 ,  G05D17/02

Abstract: An aircraft flight control system including model following control laws includes improved logic and algorithms to limit the error between a desired parameter value from the output of a model and an actual parameter value. Such logic is operable to sense the amount of said parameter error and to limit the amount of the error if it exceeds a predetermined value. The difference between the predetermined limit and the actual error is fed back to the model such that the output of the model is adjusted so that the error between the desired and actual parameter values does not exceed the predetermined value.

公开(公告)号：CA2116566A1

公开(公告)日：1993-03-18

申请号：CA2116566

申请日：1992-08-26

Applicant: UNITED TECHNOLOGIES CORP

Inventor： WRIGHT STUART C ,  DRYFOOS JAMES B

IPC: B64C13/18 ,  B64C13/50 ,  G05D1/08

Abstract: An aircraft flight control system including model following control laws includes improved logic and algorithms to limit the error between a desired parameter value from the output of a model and an actual parameter value. Such logic is operable to sense the amount of said parameter error and to limit the amount of the error if it exceeds a predetermined value. The difference between the predetermined limit and the actual error is fed back to the model such that the output of the model is adjusted so that the error between the desired and actual parameter values does not exceed the predetermined value.