EXPERIMENTAL PROGRAM TO DETERMINE THE FEASIBILITY OF USING ANALYTICAL TECHNIQUES IN ANALYZING RADIATION EFFECTS TO FLIGHT CONTROL SYSTEMS. Final Report

Radiation Effects to Flight Control Systems

IRE Transactions on Nuclear Science ◽

10.1109/tns2.1962.4315918 ◽

1962 ◽

Vol 9 (1) ◽

pp. 260-279

Author(s):

V. G. Smalley ◽

Paul Polishuk

Keyword(s):

Control Systems ◽

Flight Control ◽

Radiation Effects

Flight Control Systems: practical issues in design and implementation

10.1049/pbce057e ◽

2000 ◽

Cited By ~ 51

Keyword(s):

Control Systems ◽

Flight Control ◽

Design And Implementation

Multi-Model Approach to Parametric Robust Optimization of Digital Flight Control Systems

Journal of Automation and Information Sciences ◽

10.1615/jautomatinfscien.v36.i3.30 ◽

2004 ◽

Vol 36 (3) ◽

pp. 25-34 ◽

Cited By ~ 3

Author(s):

Anatoliy A. Tunik ◽

Elena A. Abramovich

Keyword(s):

Robust Optimization ◽

Control Systems ◽

Flight Control ◽

Model Approach

A Workstation for the Integrated Design and Simulation of Flight Control Systems

10.23919/acc.1988.4789790 ◽

1988 ◽

Cited By ~ 1

Author(s):

Richard Dean Colgren

Keyword(s):

Control Systems ◽

Flight Control ◽

Integrated Design

The Road to the Karman Line: Development of Liquid-Fueled Propulsion and Flight-Control Systems for Suborbital Launch Vehicles

AIAA Scitech 2019 Forum ◽

10.2514/6.2019-0151 ◽

2019 ◽

Author(s):

Suraj Buddhavarapu ◽

Trenton Charlson ◽

Akhil Gupta ◽

Shrivathsav Seshan

Keyword(s):

Control Systems ◽

Flight Control ◽

Launch Vehicles ◽

The Road

Verification and Validation of Real-Time Adaptive Neural Networks Using ANCT Tools and Methodologies, an Application to Intelligent Flight Control Systems F-15 Project

Infotech@Aerospace ◽

10.2514/6.2005-6997 ◽

2005 ◽

Cited By ~ 5

Author(s):

Fola Soares ◽

Kenneth Loparo ◽

John Burken ◽

Stephen Jacklin ◽

Pramod Gupta

Keyword(s):

Neural Networks ◽

Control Systems ◽

Real Time ◽

Flight Control ◽

Verification And Validation ◽

Adaptive Neural Networks

C-17 flight control systems software design

[1992] Proceedings IEEE/AIAA 11th Digital Avionics Systems Conference ◽

10.1109/dasc.1992.282097 ◽

2003 ◽

Cited By ~ 2

Author(s):

D.J. Popp ◽

R.L. Kahler

Keyword(s):

Control Systems ◽

Software Design ◽

Flight Control ◽

Systems Software

Integrating fly-by-light/power-by-wire flight control systems on transport aircraft

[1993 Proceedings] AIAA/IEEE Digital Avionics Systems Conference ◽

10.1109/dasc.1993.283507 ◽

2002 ◽

Cited By ~ 2

Author(s):

J.R. Todd ◽

J.A. Hay ◽

T. Dinh

Keyword(s):

Control Systems ◽

Flight Control ◽

Light Power ◽

Transport Aircraft

Structures and Trends in Design of Flight Control Systems for Modern Fighter Aircraft

IFAC Proceedings Volumes ◽

10.1016/s1474-6670(17)54542-5 ◽

1988 ◽

Vol 21 (18) ◽

pp. 133-138

Author(s):

S. Omlor ◽

M. Radunz

Keyword(s):

Control Systems ◽

Flight Control ◽

Fighter Aircraft

Second Paper: Failure-Survival Automatic Flight Control Systems for Aircraft with Particular Reference to a High Reliability Electrohydraulic Actuator

Proceedings of the Institution of Mechanical Engineers ◽

10.1243/pime_proc_1965_180_022_02 ◽

1965 ◽

Vol 180 (1) ◽

pp. 246-259

Author(s):

R. Ruggles

Keyword(s):

Control System ◽

Control Systems ◽

Flight Control ◽

High Reliability ◽

Supply System ◽

Design Criteria ◽

Flight Control System ◽

Advantages And Disadvantages ◽

System Configurations ◽

Very High

The author discusses some of the problems of failure-survival automatic flight control systems and suggests some basic ground rules as design criteria. The advantages and disadvantages of some of the main types of system are discussed: duplex, triplex, triple component, duplicate-monitored and quadruplex systems being covered. In particular, a quadruplex actuator is described which has been designed and developed mainly for automatic flight control system applications where a very high degrees of failure-survival capability is required. A detailed failure analysis of the various systems is carried out and the importance of the electrical and hydraulic supply system configurations and failure rates is brought out.