V. I. Grebennikov, D. Kalikhman, L. Kalikhman, S. F. Nakhov, V. Skorobogatov, E. A. Deputatova, A. Nikolaenko, R. Samitov, V. E. Kozhevnikov
{"title":"基于数字反馈精密石英摆加速度计的六轴视加速度计单元用于联盟- ms和进步- ms航天器控制系统","authors":"V. I. Grebennikov, D. Kalikhman, L. Kalikhman, S. F. Nakhov, V. Skorobogatov, E. A. Deputatova, A. Nikolaenko, R. Samitov, V. E. Kozhevnikov","doi":"10.23919/ICINS.2019.8769436","DOIUrl":null,"url":null,"abstract":"The paper studies a number of problems related to the modernization of a six-axis unit of apparent acceleration meters (originally abbreviated as the “BILU” device), which is being used as part of the Soyuz spacecraft (SC) control system since 2002. It is shown that the use of a quartz pendulum accelerometer with digital feedback expanded the functional capabilities of the device, helped to practically realize the import substitution policy, and made it possible to introduce the device to the Progress-MS control system. The developed device has passed all types of ground testing and has been supplied to RSC Energia since January 2019.","PeriodicalId":108493,"journal":{"name":"2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)","volume":"8 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2019-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":"{\"title\":\"Six-Axis Unit of Apparent Acceleration Meters Based on a Precision Quartz Pendulum Accelerometer with Digital Feedback for Control Systems of Soyuz-MS and Progress-MS Spacecrafts\",\"authors\":\"V. I. Grebennikov, D. Kalikhman, L. Kalikhman, S. F. Nakhov, V. Skorobogatov, E. A. Deputatova, A. Nikolaenko, R. Samitov, V. E. Kozhevnikov\",\"doi\":\"10.23919/ICINS.2019.8769436\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The paper studies a number of problems related to the modernization of a six-axis unit of apparent acceleration meters (originally abbreviated as the “BILU” device), which is being used as part of the Soyuz spacecraft (SC) control system since 2002. It is shown that the use of a quartz pendulum accelerometer with digital feedback expanded the functional capabilities of the device, helped to practically realize the import substitution policy, and made it possible to introduce the device to the Progress-MS control system. The developed device has passed all types of ground testing and has been supplied to RSC Energia since January 2019.\",\"PeriodicalId\":108493,\"journal\":{\"name\":\"2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)\",\"volume\":\"8 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2019-05-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"1\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.23919/ICINS.2019.8769436\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.23919/ICINS.2019.8769436","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Six-Axis Unit of Apparent Acceleration Meters Based on a Precision Quartz Pendulum Accelerometer with Digital Feedback for Control Systems of Soyuz-MS and Progress-MS Spacecrafts
The paper studies a number of problems related to the modernization of a six-axis unit of apparent acceleration meters (originally abbreviated as the “BILU” device), which is being used as part of the Soyuz spacecraft (SC) control system since 2002. It is shown that the use of a quartz pendulum accelerometer with digital feedback expanded the functional capabilities of the device, helped to practically realize the import substitution policy, and made it possible to introduce the device to the Progress-MS control system. The developed device has passed all types of ground testing and has been supplied to RSC Energia since January 2019.