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The Potential of Monitorless Control Systems of High Redundancy Efficiency
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English
Abstract
Increasing attention is being devoted to the application of various redundancy techniques to flight-control systems. The application of immediate concern in this paper is the important class of tactical military aircraft: its characteristics and its advantages.
Citation
O'Hern, E., "The Potential of Monitorless Control Systems of High Redundancy Efficiency," SAE Technical Paper 650574, 1965, https://doi.org/10.4271/650574.Also In
References
- O'Hern E. A “ An Organized Approach to the Application of Redundancy Techniques to Flight Control Systems,” Paper presented at AIAA/ASD Vehicle Design and Propulsion Meeting Wright-Patterson Air Force Base Ohio November 1963
- Derby R. M. Fleck J. J. “ Demonstration of the Application of Majority Logic for Increased Reliability in Automatic Flight Control Systems.” Prepared under Contract No. AF33 (616)-8351 by the General Electric Company, Schenectady, New York, Report, ASD-TDR-63-275 July 1963
- Moreines H. “ The Application of Redundancy to Achieve a Fail-Operative Flight Control System.” Paper presented to the Tenth Annual East Coast Conference on Aerospace Navigational Electronics, IEEE 1963
- Johnston D. “ Multiplicity Considerations Working” Paper No. 132-2, presented at Meeting No. 13, Committee No. A-18 Aerospace Vehicle Flight Control Systems, SAE Aerospace Equipment Division Houston, Texas December 1963
- Escobosa A. S. “ A Monitorless Redundancy Scheme for High Control System Reliability.” Paper prepared for Western Electric Show and Convention Los Angeles, Calif. August 1964