{"title":"Avionics system integration for the MH-53J helicopter","authors":"S. Felter, D. Hill, C.A. Smith","doi":"10.1109/DASC.1990.111264","DOIUrl":null,"url":null,"abstract":"The functions developed for the MH-53J helicopter are described, following a brief introduction of the Pave Low III system. In addition, other functions typically found in mission computers, but not in the MH-53J, are discussed. Future concepts for mission computer application are discussed. It is pointed out that the mission computer of a typical airborne platform transforms a group of independent avionic equipment into an integrated system. A centralized display system provides a common operator interface for all equipment, easing operation of the system and decluttering the instrument panel. Customized functions may be installed as required for a particular aircraft, allowing standardization of the other avionic equipment. As research progresses, the capabilities provided by the mission computer will continue to ease pilot workload and enhance the effectiveness of the avionic suite.<<ETX>>","PeriodicalId":141205,"journal":{"name":"9th IEEE/AIAA/NASA Conference on Digital Avionics Systems","volume":"11 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1990-10-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"9th IEEE/AIAA/NASA Conference on Digital Avionics Systems","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/DASC.1990.111264","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0
Abstract
The functions developed for the MH-53J helicopter are described, following a brief introduction of the Pave Low III system. In addition, other functions typically found in mission computers, but not in the MH-53J, are discussed. Future concepts for mission computer application are discussed. It is pointed out that the mission computer of a typical airborne platform transforms a group of independent avionic equipment into an integrated system. A centralized display system provides a common operator interface for all equipment, easing operation of the system and decluttering the instrument panel. Customized functions may be installed as required for a particular aircraft, allowing standardization of the other avionic equipment. As research progresses, the capabilities provided by the mission computer will continue to ease pilot workload and enhance the effectiveness of the avionic suite.<>