Hostname: page-component-586b7cd67f-gb8f7 Total loading time: 0 Render date: 2024-11-24T22:36:53.419Z Has data issue: false hasContentIssue false
  • English
  • Français

Operational data acquisition and analysis for monitoring of military aircraft usage

Published online by Cambridge University Press:  04 July 2016

J. R. Sturgeon
J. R. Sturgeon*
Affiliation:
Royal Aircraft Establishment, Farnborough
Get access Rights & Permissions [Opens in a new window]

Extract

It is usual to consider AIDS as applicable mainly to digital data; this data can usefully be divided into two main data management requirements that are unlikely to integrate for many years.

Data is required for active control of the aircraft and weapons system. This data must be immediately available to the pilot, aircraft and weapons control system; its integrity tends to demand triplex or quadruplex data sources with comprehensive Built In Test and reversionary mode operation under fault conditions. Some data also needs to be stored to aid subsequent fault diagnosis and ground maintenance but usually represents a very low data storage and analysis requirement.

Type
Research Article
Information
The Aeronautical Journal , Volume 82 , Issue 809 , May 1978 , pp. 218 - 222
Copyright
Copyright © Royal Aeronautical Society 1978 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1. Chapltn, J. A brief review of some saftey studies based on operational flight recording. AGARD Conference Proceedings 76-71.Google Scholar
2. Sturgeon, J. R. Flight data acquisition for fatigue load monitor and conservation. AGARD 32nd Structures and Materials Panel 1971.Google Scholar
3. Sturgeon, J. R. The use of accelerometers for operational load measurements in aircraft. Conference on stresses, ICE London, 1966.Google Scholar
4. Owen, E. M. Achievements in recording and analysis of civil aircraft operations 1962-69. ARC CP1181, RAE Technical Report 71034, 1971. (Unpublished.)Google Scholar
5. Taylor, J. Design and use of counting accelerometers. ARC R&M 2812, 1954.Google Scholar
6. Sturgeon, J. R. Increasing the operational effectiveness of military aircraft by flight data acquisition. RAE Technical Report 72169, 1972. (Unpublished.)Google Scholar
7. Burns, A., Thompson, J. P. and King, G. E. The application of a parametric method of fatigue load measurement to wings based on flight measurements on a Lightning Mk T5. RAE Report 77178, 1977. (Unpublished.)Google Scholar
8. Burns, A., Thompson, J. P. and Wells, E. W. The development of a parametric method of measuring fin fatigue loads based on flight measurements on a Lightning Mk T5. RAE Technical Report 76161, 1976. (Unpublished.)Google Scholar
9. Watson, P. and Dabell, B. J. Cycle counting and fatigue damage. Symposium on Statistical Aspects of Fatigue Testing. Warwick University, 1975.Google Scholar
10. Hovell, P. B. and Sturgeon, J. R. The estimation of the fatigue lives of combat aircraft from operational parametric data. ICAF Paper, Darmstat, April 1977.Google Scholar
11. Sturgeon, J. R. Influence of pilot and aircraft characteristics on structural loads in operational flight. AGARD Report 608. RAE Technical Report 73081, 1973.Google Scholar