Distributed Processing and Fiber-Optic Communications in Air Data Measurement
The application of distributed processing, fiber optics, and hardware redundancy to collecting airstream data in the digitally controlled variable-response research aircraft (VRA) at the Flight Research Laboratory of Princeton University is described. Microprocessor-controlled instrumentation packag...
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Veröffentlicht in: | IEEE transactions on aerospace and electronic systems 1983-05, Vol.AES-19 (3), p.467-473 |
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container_title | IEEE transactions on aerospace and electronic systems |
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creator | Farry, Kristin A. Stengel, Robert F. |
description | The application of distributed processing, fiber optics, and hardware redundancy to collecting airstream data in the digitally controlled variable-response research aircraft (VRA) at the Flight Research Laboratory of Princeton University is described. Microprocessor-controlled instrumentation packages in each wingtip of the aircraft collect angle-of-attack and sideslip data in digital form; after scaling, filtering, and calibrating the data, they send it to the microprocessor digital flight control system (micro-DFCS) via digital fiber-optic data links. Each wingtip package is independent of the other; therefore, the system has dual hardware redundancy. The fiver-optic link design is presented as well as a description of the calibration and communications software. Translation of the system's dual redundancy into fault tolerance is also covered. Results of preliminary flight tests are included. |
doi_str_mv | 10.1109/TAES.1983.309328 |
format | Article |
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Microprocessor-controlled instrumentation packages in each wingtip of the aircraft collect angle-of-attack and sideslip data in digital form; after scaling, filtering, and calibrating the data, they send it to the microprocessor digital flight control system (micro-DFCS) via digital fiber-optic data links. Each wingtip package is independent of the other; therefore, the system has dual hardware redundancy. The fiver-optic link design is presented as well as a description of the calibration and communications software. Translation of the system's dual redundancy into fault tolerance is also covered. 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Microprocessor-controlled instrumentation packages in each wingtip of the aircraft collect angle-of-attack and sideslip data in digital form; after scaling, filtering, and calibrating the data, they send it to the microprocessor digital flight control system (micro-DFCS) via digital fiber-optic data links. Each wingtip package is independent of the other; therefore, the system has dual hardware redundancy. The fiver-optic link design is presented as well as a description of the calibration and communications software. Translation of the system's dual redundancy into fault tolerance is also covered. Results of preliminary flight tests are included.</description><subject>Aerospace control</subject><subject>Aerospace electronics</subject><subject>Aircraft</subject><subject>Digital control</subject><subject>Distributed processing</subject><subject>Hardware</subject><subject>Optical fiber communication</subject><subject>Optical fibers</subject><subject>Packaging</subject><subject>Redundancy</subject><issn>0018-9251</issn><issn>1557-9603</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1983</creationdate><recordtype>article</recordtype><recordid>eNo9kE1LAzEURYMoWKt7wU3-wNS8vEwmWZZ-qNBSwboeMpk3EnFmSpIu_PdaKq4uF-65i8PYPYgZgLCP-_nqbQbW4AyFRWku2ATKsiqsFnjJJkKAKaws4ZrdpPT5W5VROGHbZUg5huaYqeWvcfSUUhg-uBtavg4NxWJ3yMHzxdj3xyF4l8M4JB4GPg-RL112fEsuHSP1NORbdtW5r0R3fzll7-vVfvFcbHZPL4v5pvASVC6Ux7ZqtTDKeoCONGntLTZKCeG0arV00EFnKllJ8g7BNlVjCNuuQvS6xCkT518fx5QidfUhht7F7xpEfdJRn3TUJx31Wccv8nBGAhH9zxUIaYTGHxOIW-g</recordid><startdate>198305</startdate><enddate>198305</enddate><creator>Farry, Kristin A.</creator><creator>Stengel, Robert F.</creator><general>IEEE</general><scope>AAYXX</scope><scope>CITATION</scope></search><sort><creationdate>198305</creationdate><title>Distributed Processing and Fiber-Optic Communications in Air Data Measurement</title><author>Farry, Kristin A. ; Stengel, Robert F.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c214t-4c3d7d60849c11fe6e66c93b4400a64d62a1f1f87272eca319b7b8e3df733c653</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1983</creationdate><topic>Aerospace control</topic><topic>Aerospace electronics</topic><topic>Aircraft</topic><topic>Digital control</topic><topic>Distributed processing</topic><topic>Hardware</topic><topic>Optical fiber communication</topic><topic>Optical fibers</topic><topic>Packaging</topic><topic>Redundancy</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Farry, Kristin A.</creatorcontrib><creatorcontrib>Stengel, Robert F.</creatorcontrib><collection>CrossRef</collection><jtitle>IEEE transactions on aerospace and electronic systems</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Farry, Kristin A.</au><au>Stengel, Robert F.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Distributed Processing and Fiber-Optic Communications in Air Data Measurement</atitle><jtitle>IEEE transactions on aerospace and electronic systems</jtitle><stitle>T-AES</stitle><date>1983-05</date><risdate>1983</risdate><volume>AES-19</volume><issue>3</issue><spage>467</spage><epage>473</epage><pages>467-473</pages><issn>0018-9251</issn><eissn>1557-9603</eissn><coden>IEARAX</coden><abstract>The application of distributed processing, fiber optics, and hardware redundancy to collecting airstream data in the digitally controlled variable-response research aircraft (VRA) at the Flight Research Laboratory of Princeton University is described. Microprocessor-controlled instrumentation packages in each wingtip of the aircraft collect angle-of-attack and sideslip data in digital form; after scaling, filtering, and calibrating the data, they send it to the microprocessor digital flight control system (micro-DFCS) via digital fiber-optic data links. Each wingtip package is independent of the other; therefore, the system has dual hardware redundancy. The fiver-optic link design is presented as well as a description of the calibration and communications software. Translation of the system's dual redundancy into fault tolerance is also covered. Results of preliminary flight tests are included.</abstract><pub>IEEE</pub><doi>10.1109/TAES.1983.309328</doi><tpages>7</tpages></addata></record> |
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subjects | Aerospace control Aerospace electronics Aircraft Digital control Distributed processing Hardware Optical fiber communication Optical fibers Packaging Redundancy |
title | Distributed Processing and Fiber-Optic Communications in Air Data Measurement |
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