Accession Number : ADA329056
Title : CONDUIT - A New Multidisciplinary Integration Environment for Flight Control Development.
Descriptive Note : Technical memo.,
Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMINISTRATION MOFFETT FIELD CA AMES RESEARCH CENTER
Personal Author(s) : Tischler, Mark B. ; Colbourne, Jason D. ; Morel, Mark R. ; Biezad, Daniel J. ; Levine, William S.
PDF Url : ADA329056
Report Date : JUN 1997
Pagination or Media Count : 25
Abstract : A state-of-the-art computational facility for aircraft flight control design, evaluation, and integration called CONDUIT (Control Designer's Unified Interface) has been developed. This paper describes the CONDUIT tool and case study applications to complex rotary- and fixed- wing fly-by-wire flight control problems. Control system analysis and design optimization methods are presented, including definition of design specifications and system models within CONDUIT, and the multi-objective function optimization (CONSOL-OPTCAD) used to tune the selected design parameters. Design examples are based on flight test programs for which extensive data are available for validation. CONDUIT is used to analyze baseline control laws against pertinent military handling qualities and control system specifications. In both case studies, CONDUIT successfully exploits trade-offs between forward loop and feedback dynamics to significantly improve the expected handling qualities and minimize the required actuator authority. The CONDUIT system provides a new environment for integrated control system analysis and design, and has potential for significantly reducing the time and cost of control system flight test optimization.
Descriptors : *COMPUTER PROGRAMS, *FLIGHT CONTROL SYSTEMS, *AIRCRAFT DESIGN, OPTIMIZATION, MODELS, COST ANALYSIS, SPECIFICATIONS, FLY BY WIRE CONTROL.
Subject Categories : Flight Control and Instrumentation
Computer Programming and Software
Distribution Statement : APPROVED FOR PUBLIC RELEASE