基于J-MASS的飞机实时仿真

R. Stevenson, T. Emrich, J. Jones
{"title":"基于J-MASS的飞机实时仿真","authors":"R. Stevenson, T. Emrich, J. Jones","doi":"10.1109/NAECON.1995.522023","DOIUrl":null,"url":null,"abstract":"McDonnell Douglas Aerospace (MDA) has developed a six degree-of-freedom (DOF) aircraft model that is suitable for use at various levels of simulation, from manned to interactive to all digital. The model is based on the performance of the aircraft being simulated and is used for development of flying qualities criteria or for existing simulations where high angle of attack, take-off's and landings are not required. The model is ideal for use in air combat studies where the exact performance of the model is known and real time operation is required (20 Hertz update rate). The original aircraft model was written in FORTRAN and is still in use. When a manned simulation is not needed, digital pilot logic provides stick and throttle inputs to the model. Available maneuvers include lever flight, sustained turns, waypoint following and others. This model has been rewritten in Ada and re-engineered to add additional capabilities. The model has become more object oriented, and still updates in real-time. In addition, an Ada interface has been added to the model so it is compliant with the Joint Modeling and Simulation System (J-MASS).","PeriodicalId":171918,"journal":{"name":"Proceedings of the IEEE 1995 National Aerospace and Electronics Conference. NAECON 1995","volume":"2 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1995-05-22","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":"{\"title\":\"Real time aircraft simulation using J-MASS\",\"authors\":\"R. Stevenson, T. Emrich, J. Jones\",\"doi\":\"10.1109/NAECON.1995.522023\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"McDonnell Douglas Aerospace (MDA) has developed a six degree-of-freedom (DOF) aircraft model that is suitable for use at various levels of simulation, from manned to interactive to all digital. The model is based on the performance of the aircraft being simulated and is used for development of flying qualities criteria or for existing simulations where high angle of attack, take-off's and landings are not required. The model is ideal for use in air combat studies where the exact performance of the model is known and real time operation is required (20 Hertz update rate). The original aircraft model was written in FORTRAN and is still in use. When a manned simulation is not needed, digital pilot logic provides stick and throttle inputs to the model. Available maneuvers include lever flight, sustained turns, waypoint following and others. This model has been rewritten in Ada and re-engineered to add additional capabilities. The model has become more object oriented, and still updates in real-time. In addition, an Ada interface has been added to the model so it is compliant with the Joint Modeling and Simulation System (J-MASS).\",\"PeriodicalId\":171918,\"journal\":{\"name\":\"Proceedings of the IEEE 1995 National Aerospace and Electronics Conference. NAECON 1995\",\"volume\":\"2 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1995-05-22\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"2\",\"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.1995.522023\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","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.1995.522023","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 2

摘要

麦克唐纳-道格拉斯航空航天公司(MDA)开发了一种六自由度(DOF)飞机模型,适用于从载人到交互式再到全数字的各种级别的仿真。该模型基于正在模拟的飞机的性能,用于开发飞行质量标准或用于现有的模拟,其中不需要大攻角,起飞和降落。该模型非常适合用于空战研究,其中模型的确切性能是已知的,并且需要实时操作(20赫兹更新率)。最初的飞机模型是用FORTRAN编写的,至今仍在使用。当不需要载人仿真时,数字飞行员逻辑为模型提供操纵杆和油门输入。可用的机动包括杠杆飞行、持续转弯、航路点跟随等。该模型已在Ada中重写并重新设计,以添加额外的功能。该模型变得更加面向对象,并且仍然实时更新。此外,该模型还增加了Ada接口,使其符合关节建模与仿真系统(J-MASS)。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Real time aircraft simulation using J-MASS
McDonnell Douglas Aerospace (MDA) has developed a six degree-of-freedom (DOF) aircraft model that is suitable for use at various levels of simulation, from manned to interactive to all digital. The model is based on the performance of the aircraft being simulated and is used for development of flying qualities criteria or for existing simulations where high angle of attack, take-off's and landings are not required. The model is ideal for use in air combat studies where the exact performance of the model is known and real time operation is required (20 Hertz update rate). The original aircraft model was written in FORTRAN and is still in use. When a manned simulation is not needed, digital pilot logic provides stick and throttle inputs to the model. Available maneuvers include lever flight, sustained turns, waypoint following and others. This model has been rewritten in Ada and re-engineered to add additional capabilities. The model has become more object oriented, and still updates in real-time. In addition, an Ada interface has been added to the model so it is compliant with the Joint Modeling and Simulation System (J-MASS).
求助全文
通过发布文献求助,成功后即可免费获取论文全文。 去求助
来源期刊
自引率
0.00%
发文量
0
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:604180095
Book学术官方微信