Accession Number : AD0889266

Title :   Demonstration of Combined Reliability Prediction and Verification Techniques to a Typical Flight Control System. Volume III. Tabular System Reliability Analysis Computer Output Data Sheets.

Descriptive Note : Final rept. 15 Feb 70-15 Feb 71,

Corporate Author : BATTELLE MEMORIAL INST COLUMBUS OH COLUMBUS LABS

Personal Author(s) : Blazek, R. H. ; Thomas, R. E. ; Thatcher, R. K. ; Easterday, J. L.

Report Date : OCT 1971

Pagination or Media Count : 138

Abstract : The report is Volume 3 of the final report on the subject contract consisting of computer printouts illustrating the actual format and output from the TASRA (Tabular System Reliability Analysis) program. These data are in support of the basic reliability and safety analysis of the pitch axis of the F-111 flight control system discussed in Volume 1 of this final report. Reliability and safety prediction calculations are tabulated for operating times of 2, 10, 100, and 1000 hours. (Author)

Descriptors :   *FLIGHT CONTROL SYSTEMS), (*FLIGHT CONTROL SYSTEMS, NUMERICAL ANALYSIS), (*JET FIGHTERS, ADAPTIVE CONTROL SYSTEMS, PITCH(MOTION), AVIATION SAFETY, RELIABILITY, PREDICTIONS, INPUT OUTPUT DEVICES, TABLES(DATA).

Subject Categories : Attack and Fighter Aircraft
      Computer Hardware

Distribution Statement : APPROVED FOR PUBLIC RELEASE