{"title":"The airborne intelligent pilot motor actions decisions support system and its methodological foundation","authors":"O. Yakimenko","doi":"10.1109/NAECON.1995.521979","DOIUrl":null,"url":null,"abstract":"Deals with the design ofan airborne intelligent pilot action level decisions support system, which provides a multifunctional cockpit display of optimal flight trajectory in the image of \"road in the sky\". This system of intelligent support of pilot's operation during maneuvering at \"standard\" trajectories (such as climb-up, flight on a route, battle maneuvering, returning to the base, landing etc.), is a part of a universal pilot support system. The general structure of such a system, its input and output signals, the way of boundary condition set, the method of optimization task solution (based on approximation of the trajectory by a special polynomial) and on-board trajectories formation procedure, are discussed.","PeriodicalId":171918,"journal":{"name":"Proceedings of the IEEE 1995 National Aerospace and Electronics Conference. NAECON 1995","volume":"216 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1995-05-22","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"4","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Proceedings of the IEEE 1995 National Aerospace and Electronics Conference. NAECON 1995","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/NAECON.1995.521979","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 4
Abstract
Deals with the design ofan airborne intelligent pilot action level decisions support system, which provides a multifunctional cockpit display of optimal flight trajectory in the image of "road in the sky". This system of intelligent support of pilot's operation during maneuvering at "standard" trajectories (such as climb-up, flight on a route, battle maneuvering, returning to the base, landing etc.), is a part of a universal pilot support system. The general structure of such a system, its input and output signals, the way of boundary condition set, the method of optimization task solution (based on approximation of the trajectory by a special polynomial) and on-board trajectories formation procedure, are discussed.