The Development Of The Conduit Advanced Control System Design And Evaluation Interface With A Case Study Application To An Advanced Fly By Wire Helicopter Design
Download The Development Of The Conduit Advanced Control System Design And Evaluation Interface With A Case Study Application To An Advanced Fly By Wire Helicopter Design PDF/ePub or read online books in Mobi eBooks. Click Download or Read Online button to get The Development Of The Conduit Advanced Control System Design And Evaluation Interface With A Case Study Application To An Advanced Fly By Wire Helicopter Design book now. This website allows unlimited access to, at the time of writing, more than 1.5 million titles, including hundreds of thousands of titles in various foreign languages.
CONDUIT: A New Multidisciplinary Integration Environment for Flight Control Development
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.
The Development of the Conduit Advanced Control System Design and Evaluation Interface with a Case Study Application to an Advanced Fly by Wire Helicopter Design
Author: National Aeronautics and Space Administration (NASA)
language: en
Publisher: Createspace Independent Publishing Platform
Release Date: 2018-06-11
This report details the development and use of CONDUIT (Control Designer's Unified Interface). CONDUIT is a design tool created at Ames Research Center for the purpose of evaluating and optimizing aircraft control systems against handling qualities. Three detailed design problems addressing the RASCAL UH-60A Black Hawk are included in this report to show the application of CONDUIT to helicopter control system design.Colbourne, JasonAmes Research CenterAIRCRAFT CONTROL; CONTROL SYSTEMS DESIGN; DESIGN ANALYSIS; COMPUTER PROGRAMS; HELICOPTER CONTROL; PIPES (TUBES); FLY BY WIRE CONTROL