{"title":"Heli/SITAN: a terrain referenced navigation algorithm for helicopters","authors":"J. Hollowell","doi":"10.1109/PLANS.1990.66236","DOIUrl":null,"url":null,"abstract":"Heli/SITAN is a terrain referenced navigation algorithm that utilizes radar altimeter ground clearance measurements in combination with a conventional navigation system and a stored digital terrain elevation map to estimate a helicopter's position accurately. Multiple model adaptive estimation techniques are used, and a bank of single-state Kalman filters is used to ensure that reliable position estimates are obtained even in the face of large initial position errors. A real-time implementation of the algorithm was tested aboard a US Army UH-1 helicopter equipped with a Singer-Kearfott Doppler velocity sensor and a Litton LR-80 strapdown attitude and heading reference system (AHRS). The median radial error of the position fixes provided in real time by this implementation was less than 50 m for a variety of mission profiles. Although Heli/SITAN was demonstrated on a helicopter equipped with a Doppler aided AHRS, the extension to other types of aircraft and navigation systems is straightforward.<<ETX>>","PeriodicalId":156436,"journal":{"name":"IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences","volume":"1 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1990-03-20","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"95","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/PLANS.1990.66236","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 95
Abstract
Heli/SITAN is a terrain referenced navigation algorithm that utilizes radar altimeter ground clearance measurements in combination with a conventional navigation system and a stored digital terrain elevation map to estimate a helicopter's position accurately. Multiple model adaptive estimation techniques are used, and a bank of single-state Kalman filters is used to ensure that reliable position estimates are obtained even in the face of large initial position errors. A real-time implementation of the algorithm was tested aboard a US Army UH-1 helicopter equipped with a Singer-Kearfott Doppler velocity sensor and a Litton LR-80 strapdown attitude and heading reference system (AHRS). The median radial error of the position fixes provided in real time by this implementation was less than 50 m for a variety of mission profiles. Although Heli/SITAN was demonstrated on a helicopter equipped with a Doppler aided AHRS, the extension to other types of aircraft and navigation systems is straightforward.<>