Add to ORKGThe research is reported on the problems of failure detection and reliable system design for digital aircraft control systems. Failure modes, cross detection probability, wrong time detection, application of performance tools, and the GLR computer package are discussed
Theory and techniques for design, analysis, and fault diagnosis of reliable spacecraft data system
A highly-reliable, fault-tolerant reconfigurable computer system for aircraft applications was devel...
The ability of a pilot to reconfigure the control surfaces on an airplane after a failure, allowing ...
Includes bibliographical references.Originally presented as author's thesis (M.S.--Masschusetts Insi...
The application of the Generalized Likelihood Ratio technique to the detection and identification of...
The analysis and design of complex multivariable reliable control systems are considered. High perfo...
A new sensor/actuator failure analysis technique for turbofan jet engines was developed. Three phase...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1973....
Articles are presented on pilot performance in zero-visibility precision approach, failure detection...
This report presents a preliminary design for flight testing the FINDS (Fault Inferring Nonlinear De...
Failure detection and identification logic for a fault-tolerant longitudinal control system were inv...
Prepared for the Office of Naval Research on ONR Contract no. N00014-77-C-0224. Issued by: M.I.T. El...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.In...
The coupling of expert systems and control design and analysis techniques are documented to provide ...
A number of methods for the detection of abrupt changes (such as failures) in stochastic dynamical s...
Theory and techniques for design, analysis, and fault diagnosis of reliable spacecraft data system
A highly-reliable, fault-tolerant reconfigurable computer system for aircraft applications was devel...
The ability of a pilot to reconfigure the control surfaces on an airplane after a failure, allowing ...
Includes bibliographical references.Originally presented as author's thesis (M.S.--Masschusetts Insi...
The application of the Generalized Likelihood Ratio technique to the detection and identification of...
The analysis and design of complex multivariable reliable control systems are considered. High perfo...
A new sensor/actuator failure analysis technique for turbofan jet engines was developed. Three phase...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1973....
Articles are presented on pilot performance in zero-visibility precision approach, failure detection...
This report presents a preliminary design for flight testing the FINDS (Fault Inferring Nonlinear De...
Failure detection and identification logic for a fault-tolerant longitudinal control system were inv...
Prepared for the Office of Naval Research on ONR Contract no. N00014-77-C-0224. Issued by: M.I.T. El...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.In...
The coupling of expert systems and control design and analysis techniques are documented to provide ...
A number of methods for the detection of abrupt changes (such as failures) in stochastic dynamical s...
Theory and techniques for design, analysis, and fault diagnosis of reliable spacecraft data system
A highly-reliable, fault-tolerant reconfigurable computer system for aircraft applications was devel...
The ability of a pilot to reconfigure the control surfaces on an airplane after a failure, allowing ...