先进巡航导弹制导系统描述

Proceedings of the IEEE 1993 National Aerospace and Electronics Conference-NAECON 1993 Pub Date : 1993-05-24 DOI:10.1109/NAECON.1993.290941

S. Hicks

{"title":"先进巡航导弹制导系统描述","authors":"S. Hicks","doi":"10.1109/NAECON.1993.290941","DOIUrl":null,"url":null,"abstract":"This paper provides a functional description of the navigation and guidance system in the Advanced Cruise Missile (ACM), one of the Air Force's newest stealth missiles. It also discusses some of the areas of improvement over the Air Launched Cruise Missile (ALCM). The Kalman Filter design accommodates velocity updates, including lateral velocities, and a nominal number of position updates from terrain correlation matching (TERCOM) to achieve a high accuracy, long range mission.<<ETX>>","PeriodicalId":183796,"journal":{"name":"Proceedings of the IEEE 1993 National Aerospace and Electronics Conference-NAECON 1993","volume":"4 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1993-05-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"13","resultStr":"{\"title\":\"Advanced Cruise Missile guidance system description\",\"authors\":\"S. Hicks\",\"doi\":\"10.1109/NAECON.1993.290941\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"This paper provides a functional description of the navigation and guidance system in the Advanced Cruise Missile (ACM), one of the Air Force's newest stealth missiles. It also discusses some of the areas of improvement over the Air Launched Cruise Missile (ALCM). The Kalman Filter design accommodates velocity updates, including lateral velocities, and a nominal number of position updates from terrain correlation matching (TERCOM) to achieve a high accuracy, long range mission.<<ETX>>\",\"PeriodicalId\":183796,\"journal\":{\"name\":\"Proceedings of the IEEE 1993 National Aerospace and Electronics Conference-NAECON 1993\",\"volume\":\"4 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1993-05-24\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"13\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Proceedings of the IEEE 1993 National Aerospace and Electronics Conference-NAECON 1993\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/NAECON.1993.290941\",\"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 1993 National Aerospace and Electronics Conference-NAECON 1993","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/NAECON.1993.290941","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}

引用次数: 13

摘要

本文介绍了空军最新隐身导弹之一的先进巡航导弹(ACM)导航制导系统的功能描述。讨论了对空射巡航导弹(ALCM)的改进。卡尔曼滤波器设计适应速度更新，包括横向速度，以及地形相关匹配(TERCOM)的标称数量的位置更新，以实现高精度，远程任务。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

查看原文本刊更多论文

Advanced Cruise Missile guidance system description

This paper provides a functional description of the navigation and guidance system in the Advanced Cruise Missile (ACM), one of the Air Force's newest stealth missiles. It also discusses some of the areas of improvement over the Air Launched Cruise Missile (ALCM). The Kalman Filter design accommodates velocity updates, including lateral velocities, and a nominal number of position updates from terrain correlation matching (TERCOM) to achieve a high accuracy, long range mission.<>

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

Proceedings of the IEEE 1993 National Aerospace and Electronics Conference-NAECON 1993

自引率

0.00%

发文量