Primary Flight Control Hydraulic Actuation System Interface Definition PDF Download
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Author | : A-6A3 Flight Control and Vehicle Management Systems Cmt |
Publisher | : |
Total Pages | : 0 |
Release | : 2015 |
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Download Primary Flight Control Hydraulic Actuation System Interface Definition Book in PDF, ePub and Kindle
This SAE Aerospace Information Report (AIR) provides a description of the interfaces and their requirements for generic and specific hydraulic actuation systems used in the flight control systems of manned aircraft. Included are the basic control system characteristics and functional requirements, and the essential interfaces (structural, mechanical, hydraulic power, control input, status monitoring, and environment). Major design issues, requirements, and other considerations are presented and discussed. This document contains information addressing aspects of technology that are not currently undergoing substantial development.
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Total Pages | : 49 |
Release | : 2015 |
Genre | : Aerospace engineering |
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Download Primary Flight Control Hydraulic Actuation System Interface Definition Book in PDF, ePub and Kindle
"This document primarily provides an introductory treatment of the more relevant issues regarding system interfaces. The information may be used to support the preparation of an interface specification. Considerations for use in making trades and evaluation of several types of interfaces included. More detailed information relating to specific interface design is left to other SAE documentation."--Foreword.
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Total Pages | : 512 |
Release | : 1974 |
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Download Digital Flight Control Actuation System Study Book in PDF, ePub and Kindle
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Total Pages | : 30 |
Release | : 1997 |
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Download CONDUIT: A New Multidisciplinary Integration Environment for Flight Control Development Book in PDF, ePub and Kindle
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.
Author | : Eugene T. Raymond |
Publisher | : |
Total Pages | : 270 |
Release | : 1993 |
Genre | : Technology & Engineering |
ISBN | : 9781560913764 |
Download Aircraft Flight Control Actuation System Design Book in PDF, ePub and Kindle
Author | : Yu Liu |
Publisher | : Springer Nature |
Total Pages | : 642 |
Release | : 2023-07-04 |
Genre | : Technology & Engineering |
ISBN | : 3031288599 |
Download Advances in Reliability and Maintainability Methods and Engineering Applications Book in PDF, ePub and Kindle
This comprehensive book brings together the latest developments in reliability and maintainability methods from leading research groups globally. Covering a diverse range of subject areas, from mechanical systems to cyber-physical systems, the book offers both theoretical advancements and practical applications in various industries. With a focus on reliability modelling, reliability analysis, reliability design, maintenance optimization, warranty policy, prognostics and health management, this book appeals to academic and industrial professionals in the field of reliability engineering and beyond. It features real-world case studies from turbofan engines bearings, industrial robots, wireless networks, aircraft actuation systems, and more. This book is ideal for engineers, scientists, and graduate students in reliability, maintainability, design optimization, prognostics and health management, and applied probability and statistics.
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Total Pages | : 516 |
Release | : 1974 |
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Download NASA Technical Note Book in PDF, ePub and Kindle
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Total Pages | : 300 |
Release | : 1995 |
Genre | : Aeronautics |
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Download Scientific and Technical Aerospace Reports Book in PDF, ePub and Kindle
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Total Pages | : 178 |
Release | : 1986 |
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Download Research and Development of Aircraft Control Actuation Systems Book in PDF, ePub and Kindle
This report describes the design and test of a multipurpose actuation test rig to be used for loaded evaluation of actuation systems with rotary outputs and/or integrated as part of wing structure. It also describes a hydromechanical flutter damping module for an F-4 stabilator actuator. The module incorporates design improvements based on previous test results. Laboratory tests results on the improved module are presented. Development and test results of a linear force motor based upon a moving magnet concept, and the measured performance characteristics of the concept over a range of parameter variations are presented. A method of force enhancement for direct drive force motors and the corresponding test results applied to a moving coil force motor are described. The concept is based upon applying a limited time duration pulse to the force motor in order to increase the force output when required. The logic technique used to initiate the pulse application is presented. Applying a digital computer as a controller for an analog electrohydraulic control system requires consideration of the interface used. The effect of a pulse width modulation interface on the life of analog electrohydraulic hardware is presented. There is a potential for reducing the pumping capacity of an aircraft's flight control hydraulic system by using accumulators to store hydraulic energy. The results of a study using this approach and an F-16 simulation are presented. Keywords: Digital interface; Energy storage; Flight control hydraulics; Force enhancement, Flutter suppression.
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Total Pages | : 212 |
Release | : 1992 |
Genre | : Aeronautics |
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Download NASA Technical Memorandum Book in PDF, ePub and Kindle