R. Mullen, B. Tanju, M. May, C. Mannis, C. Sives, M. Engelhart
{"title":"Integration of full scale development aircraft GPS user equipment (AN/ARN-151) with Doppler radar systems","authors":"R. Mullen, B. Tanju, M. May, C. Mannis, C. Sives, M. Engelhart","doi":"10.1109/PLANS.1992.185855","DOIUrl":null,"url":null,"abstract":"Tests of a full-scale development aircraft GPS (Global Positioning System) user equipment (AN/ARN-151) Receiver-3A integrated with a simulated DRS (Doppler radar system) via a mission computer MIL-STD-1553B bus were performed. Test conditions were particularized to an SH-60F platform as a baseline; specific test conclusions should not be generalized to embedded GPS/DRS suites or other GPS/DRS integrations. The simulation results indicate that overall benefits in the areas of satellite acquisition/reacquisition, antijamming performance, and performance during degraded satellite availability accrue when the Receiver-3A is integrated with the Doppler system. Without Doppler aiding, the Receiver-3A under conditions of jamming-to-signal ratios greater than 42 dB or under conditions of two or less satellite availability would potentially have an unbounded position error growth. With Doppler aiding, the acquisition/reacquisition process is improved, the antijamming margin is increased by at least 10 dB, and position error growth is always bounded by (at worst) Doppler position error growth.<<ETX>>","PeriodicalId":422101,"journal":{"name":"IEEE PLANS 92 Position Location and Navigation Symposium Record","volume":"1 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1992-03-23","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"IEEE PLANS 92 Position Location and Navigation Symposium Record","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/PLANS.1992.185855","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
Tests of a full-scale development aircraft GPS (Global Positioning System) user equipment (AN/ARN-151) Receiver-3A integrated with a simulated DRS (Doppler radar system) via a mission computer MIL-STD-1553B bus were performed. Test conditions were particularized to an SH-60F platform as a baseline; specific test conclusions should not be generalized to embedded GPS/DRS suites or other GPS/DRS integrations. The simulation results indicate that overall benefits in the areas of satellite acquisition/reacquisition, antijamming performance, and performance during degraded satellite availability accrue when the Receiver-3A is integrated with the Doppler system. Without Doppler aiding, the Receiver-3A under conditions of jamming-to-signal ratios greater than 42 dB or under conditions of two or less satellite availability would potentially have an unbounded position error growth. With Doppler aiding, the acquisition/reacquisition process is improved, the antijamming margin is increased by at least 10 dB, and position error growth is always bounded by (at worst) Doppler position error growth.<>