Pub Date : 2017-03-01DOI: 10.17238/ISSN2409-0239.2017.1.89
Y. Baturin
. This article considers the period of the birth of the space industry in the Soviet Union prior to the adoption in May 1946 of the USSR Council of Ministers Resolution “Issues of missile weapons” which is considered to be the beginning of its history. It gives little-known information about the joint Anglo-American-Soviet military-technical expedition to Poland during the fighting to search for the fallen German V-2 rockets. The structure of the search and the export of samples of missile technology, technical documentation and rocket-specialists from Germany to the Soviet Union is described. Investigated in detail is the process of forming of the People’s Commissariat, which should be entrusted with the production of missile weapons.
{"title":"The Birth of Russian Rocket and Space Industry","authors":"Y. Baturin","doi":"10.17238/ISSN2409-0239.2017.1.89","DOIUrl":"https://doi.org/10.17238/ISSN2409-0239.2017.1.89","url":null,"abstract":". This article considers the period of the birth of the space industry in the Soviet Union prior to the adoption in May 1946 of the USSR Council of Ministers Resolution “Issues of missile weapons” which is considered to be the beginning of its history. It gives little-known information about the joint Anglo-American-Soviet military-technical expedition to Poland during the fighting to search for the fallen German V-2 rockets. The structure of the search and the export of samples of missile technology, technical documentation and rocket-specialists from Germany to the Soviet Union is described. Investigated in detail is the process of forming of the People’s Commissariat, which should be entrusted with the production of missile weapons.","PeriodicalId":436954,"journal":{"name":"Rocket-Space Device Engineering and Information Systems","volume":"27 10 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2017-03-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"117025553","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2017-03-01DOI: 10.17238/issn2409-0239.2017.1.46
D. Ermolaev, A. Talanov, V. A. Romanyuk
{"title":"Prospects of Terahertz Frequencies Application","authors":"D. Ermolaev, A. Talanov, V. A. Romanyuk","doi":"10.17238/issn2409-0239.2017.1.46","DOIUrl":"https://doi.org/10.17238/issn2409-0239.2017.1.46","url":null,"abstract":"","PeriodicalId":436954,"journal":{"name":"Rocket-Space Device Engineering and Information Systems","volume":"164 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2017-03-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"122926343","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2017-03-01DOI: 10.17238/issn2409-0239.2017.1.3
V. Filimonov, V. I. Tislenko, V. Lebedev, A. P. Kravets
This paper describes the analysis of a RMS error of the state vector estimations, which contain the current coordinates and velocity of a spacecraft (SC). Moreover, it includes shift of the time scale and frequency of the onboard reference generator (RG). The estimates are transferred to the output of the navigation computer, where they are formed. The processing algorithm uses observation data in the form of pseudoranges and pseudovelocities according to several GNSS SC. The mathematical state model takes into account the presence of random fluctuations based on the SC acceleration components caused by SC orbit variations. Observation channels contain random errors in the form of white Gaussian noise. The variation model of RG frequency corresponds to the model of the rubidium frequency standard. The article shows that the sigma point Kalman filter provides a positioning RMS error of less than 1 m, a velocity model error of less than 0.01 m/s, a time scale shift of less than 1.9 ns, and a frequency instability of less than 3 · 10−13, in conditions when SC moves in a highly elliptical orbit (HEO) at high values of GDOP and weak signals. The algorithm does not lose its efficiency even at incomplete constellations of GNSS SC up to several minutes.
{"title":"Sigma Point Algorithm of the Kalman Filter in Spacecraft Autonomous Navigation","authors":"V. Filimonov, V. I. Tislenko, V. Lebedev, A. P. Kravets","doi":"10.17238/issn2409-0239.2017.1.3","DOIUrl":"https://doi.org/10.17238/issn2409-0239.2017.1.3","url":null,"abstract":"This paper describes the analysis of a RMS error of the state vector estimations, which contain the current coordinates and velocity of a spacecraft (SC). Moreover, it includes shift of the time scale and frequency of the onboard reference generator (RG). The estimates are transferred to the output of the navigation computer, where they are formed. The processing algorithm uses observation data in the form of pseudoranges and pseudovelocities according to several GNSS SC. The mathematical state model takes into account the presence of random fluctuations based on the SC acceleration components caused by SC orbit variations. Observation channels contain random errors in the form of white Gaussian noise. The variation model of RG frequency corresponds to the model of the rubidium frequency standard. The article shows that the sigma point Kalman filter provides a positioning RMS error of less than 1 m, a velocity model error of less than 0.01 m/s, a time scale shift of less than 1.9 ns, and a frequency instability of less than 3 · 10−13, in conditions when SC moves in a highly elliptical orbit (HEO) at high values of GDOP and weak signals. The algorithm does not lose its efficiency even at incomplete constellations of GNSS SC up to several minutes.","PeriodicalId":436954,"journal":{"name":"Rocket-Space Device Engineering and Information Systems","volume":"54 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2017-03-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"129876604","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2017-03-01DOI: 10.17238/issn2409-0239.2017.1.84
V. Selivanov, Yu.M. Gekhtin, S. Ryabkov
{"title":"Multiangle Video Polarimeter for Optical Range","authors":"V. Selivanov, Yu.M. Gekhtin, S. Ryabkov","doi":"10.17238/issn2409-0239.2017.1.84","DOIUrl":"https://doi.org/10.17238/issn2409-0239.2017.1.84","url":null,"abstract":"","PeriodicalId":436954,"journal":{"name":"Rocket-Space Device Engineering and Information Systems","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2017-03-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"129624002","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2017-03-01DOI: 10.17238/ISSN2409-0239.2017.1.61
V. Vorontsov
Analysis is made available of capabilities for improving data reliability by integrating the noiseless coding techniques (decoding) that, above all, is recommended by CCSDS, and the diversity reception techniques described in the Orange Book CCSDS 551.1-O-1 “Correlated Data Generation”. The integration approach described in the aforesaid Orange Book is detailed. Demonstrative examples and simple calculations are cited to illustrate that data reliability is substantially improved. Herewith, the reasons are given for selecting the optimal integration method; otherwise, it could result in the degradation of reliability (the necessary condition for making the adequate choice – the technique conformity to the interference situation). It is proposed to make better use of the diversity reception techniques (obviously underappreciated by the CCSDS community).
{"title":"Reliability Improvement Through Making the Most Use of Data Diverse Reception Capabilities","authors":"V. Vorontsov","doi":"10.17238/ISSN2409-0239.2017.1.61","DOIUrl":"https://doi.org/10.17238/ISSN2409-0239.2017.1.61","url":null,"abstract":"Analysis is made available of capabilities for improving data reliability by integrating the noiseless coding techniques (decoding) that, above all, is recommended by CCSDS, and the diversity reception techniques described in the Orange Book CCSDS 551.1-O-1 “Correlated Data Generation”. The integration approach described in the aforesaid Orange Book is detailed. Demonstrative examples and simple calculations are cited to illustrate that data reliability is substantially improved. Herewith, the reasons are given for selecting the optimal integration method; otherwise, it could result in the degradation of reliability (the necessary condition for making the adequate choice – the technique conformity to the interference situation). It is proposed to make better use of the diversity reception techniques (obviously underappreciated by the CCSDS community).","PeriodicalId":436954,"journal":{"name":"Rocket-Space Device Engineering and Information Systems","volume":"16 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2017-03-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"131177832","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2016-12-01DOI: 10.17238/ISSN2409-0239.2016.4.80
E. Ivoylov, S. Slobodyan, A. A. Tsupin, V. Deeva
. The performance potential of optical and laser technologies offers the great challenge of using them in many industries and areas of science effectively. For example, high intensity precise directional electromagnetic radiation is factored into the test program with the use of a portable high-precision system. The most significantly factor is that laser targeting is used for the detection and tracking of dynamic objects of any shapes. To expand the field of vision the laser systems is installed in multimotion control platform. In this paper we propose a model of a N -degree-of-freedom motion platform. Also we investigate, using computational modeling and simulation, the potential of the 1 D -motion platform to expand the field of vision of the laser systems and we receive influence from other variables.
{"title":"Simulation of the Mechatronic Dynamic Platform Equipped with Laser Navigation System to Operate the Spacecrafts","authors":"E. Ivoylov, S. Slobodyan, A. A. Tsupin, V. Deeva","doi":"10.17238/ISSN2409-0239.2016.4.80","DOIUrl":"https://doi.org/10.17238/ISSN2409-0239.2016.4.80","url":null,"abstract":". The performance potential of optical and laser technologies offers the great challenge of using them in many industries and areas of science effectively. For example, high intensity precise directional electromagnetic radiation is factored into the test program with the use of a portable high-precision system. The most significantly factor is that laser targeting is used for the detection and tracking of dynamic objects of any shapes. To expand the field of vision the laser systems is installed in multimotion control platform. In this paper we propose a model of a N -degree-of-freedom motion platform. Also we investigate, using computational modeling and simulation, the potential of the 1 D -motion platform to expand the field of vision of the laser systems and we receive influence from other variables.","PeriodicalId":436954,"journal":{"name":"Rocket-Space Device Engineering and Information Systems","volume":"9 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-12-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"126717951","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2016-12-01DOI: 10.17238/issn2409-0239.2016.4.48
А. Romanov
. The article offers an analysis of the main approaches to the building of a scientific, technical and technological base in space device engineering organizations. It is noted that presently in the leading corporations of aerospace, the research and development is mainly conducted in the major corporate centers that implement the principles of systems engineering. The main innovation planning documents are the technological roadmaps for critical areas, on the basis of which the advanced space technology development projects, that include the main stages of the product life cycle, are created. The availability engineering of the technological innovation in the company AIRBUS DEFENCE AND SPACE is considered. It is noted that the costs of research and development correspond to approximately 5% of the company’s total funding. The concept of the corporate center for research and development in the field of space device engineering is suggested. The main technological trends in the development of advanced service and target devices in the integrated structure of the Joint Stock Company “Russian Space Systems” are discussed. The results are presented in the summary table of critical device (system) engineering technologies.
{"title":"Development of a Science and Technology Basis for Creation of Advanced Space Engineering Technologies","authors":"А. Romanov","doi":"10.17238/issn2409-0239.2016.4.48","DOIUrl":"https://doi.org/10.17238/issn2409-0239.2016.4.48","url":null,"abstract":". The article offers an analysis of the main approaches to the building of a scientific, technical and technological base in space device engineering organizations. It is noted that presently in the leading corporations of aerospace, the research and development is mainly conducted in the major corporate centers that implement the principles of systems engineering. The main innovation planning documents are the technological roadmaps for critical areas, on the basis of which the advanced space technology development projects, that include the main stages of the product life cycle, are created. The availability engineering of the technological innovation in the company AIRBUS DEFENCE AND SPACE is considered. It is noted that the costs of research and development correspond to approximately 5% of the company’s total funding. The concept of the corporate center for research and development in the field of space device engineering is suggested. The main technological trends in the development of advanced service and target devices in the integrated structure of the Joint Stock Company “Russian Space Systems” are discussed. The results are presented in the summary table of critical device (system) engineering technologies.","PeriodicalId":436954,"journal":{"name":"Rocket-Space Device Engineering and Information Systems","volume":"21 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-12-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"131016688","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2016-12-01DOI: 10.17238/issn2409-0239.2016.4.74
O. A. Alekseev, E. I. Tsadikovskiy
. The article reviews the methodology of integrating space information resources for short-term forecasting of natural and anthropogenic emergencies. The purpose of such integrating is to increase the success rate, accuracy and timeliness of emergency forecasts with limited expenses connected with the improvement of the monitoring system for emergency forecasting. The target of the research is a system for monitoring and forecasting of natural and man-caused emergencies. The scope of the research covers integration types of information resources in a system that are determined by integration of data, knowledge and the stages of monitoring information processing. Particularities of each integration type are illustrated with Petri nets. A selection mechanism is suggested for possible multiple variants of resources integration, determined by the integration types, the number of system elements and the number of estimated parameters. The logic of the mechanism is reflective of development possibilities of the system and of the realization of its integrated variants. It is emphasized that the integration of information resources of the emergency monitoring and forecasting system should be started with integration of data and knowledge on the previous processing stages. Potential result is a monitoring and forecasting system with few branches that includes all stages of processing of the monitoring information.
{"title":"Methodological Aspects of Information Resources Integration in Space-Based Facilities for Emergency Monitoring and Forecasting","authors":"O. A. Alekseev, E. I. Tsadikovskiy","doi":"10.17238/issn2409-0239.2016.4.74","DOIUrl":"https://doi.org/10.17238/issn2409-0239.2016.4.74","url":null,"abstract":". The article reviews the methodology of integrating space information resources for short-term forecasting of natural and anthropogenic emergencies. The purpose of such integrating is to increase the success rate, accuracy and timeliness of emergency forecasts with limited expenses connected with the improvement of the monitoring system for emergency forecasting. The target of the research is a system for monitoring and forecasting of natural and man-caused emergencies. The scope of the research covers integration types of information resources in a system that are determined by integration of data, knowledge and the stages of monitoring information processing. Particularities of each integration type are illustrated with Petri nets. A selection mechanism is suggested for possible multiple variants of resources integration, determined by the integration types, the number of system elements and the number of estimated parameters. The logic of the mechanism is reflective of development possibilities of the system and of the realization of its integrated variants. It is emphasized that the integration of information resources of the emergency monitoring and forecasting system should be started with integration of data and knowledge on the previous processing stages. Potential result is a monitoring and forecasting system with few branches that includes all stages of processing of the monitoring information.","PeriodicalId":436954,"journal":{"name":"Rocket-Space Device Engineering and Information Systems","volume":"54 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-12-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114575359","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2016-12-01DOI: 10.17238/ISSN2409-0239.2016.4.89
Yu.Yu. Gulin, A. Ryabev, M. Gorchichko
. This article discusses the ongoing development of SPICE-models of the complementary bipolar transistors (CBT) with account for dose radiation effects. The conducted research included exposing the transistors to the source of gamma rays. The ex-perimental characteristics, reflecting the degradation parameters of the bipolar transistors under the influence of the accumulated dose of radiation are attained, as well as at the extracted parameters of the SPICE-model. Based on the extracted parameters, a SPICE-model of complementary bipolar transistors has been developed, with account for the radioactive degradation with the dosage absorbed ranging from 0 to 100 krad (Si).
{"title":"Development of SPICE-models of the Complementary Bipolar Transistors with Account for Dose Effect","authors":"Yu.Yu. Gulin, A. Ryabev, M. Gorchichko","doi":"10.17238/ISSN2409-0239.2016.4.89","DOIUrl":"https://doi.org/10.17238/ISSN2409-0239.2016.4.89","url":null,"abstract":". This article discusses the ongoing development of SPICE-models of the complementary bipolar transistors (CBT) with account for dose radiation effects. The conducted research included exposing the transistors to the source of gamma rays. The ex-perimental characteristics, reflecting the degradation parameters of the bipolar transistors under the influence of the accumulated dose of radiation are attained, as well as at the extracted parameters of the SPICE-model. Based on the extracted parameters, a SPICE-model of complementary bipolar transistors has been developed, with account for the radioactive degradation with the dosage absorbed ranging from 0 to 100 krad (Si).","PeriodicalId":436954,"journal":{"name":"Rocket-Space Device Engineering and Information Systems","volume":"104 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-12-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"124829962","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2016-12-01DOI: 10.17238/ISSN2409-0239.2016.4.22
A. Petrukovich, O. Nikiforov
. This article reports on the international experience of scientific satellite launches for magnetosphere and ionosphere plasma research with an emphasis on the use of small satellites. For magnetospheric studies, satellites weighting 100–1000 kg are mainly used. In low Earth orbit (convenient for ionospheric studies) micro- and nanosatellites have dominated in the recent years. The paper formulates scientific objectives for the future micro- and nanosatellites in various orbits, as well as approaches to the assessment of their effectiveness. The paper discusses the common problems of this development field and their possible solutions, both as a whole and for the Russian space program in particular.
{"title":"Small Satellites for Scientific Research","authors":"A. Petrukovich, O. Nikiforov","doi":"10.17238/ISSN2409-0239.2016.4.22","DOIUrl":"https://doi.org/10.17238/ISSN2409-0239.2016.4.22","url":null,"abstract":". This article reports on the international experience of scientific satellite launches for magnetosphere and ionosphere plasma research with an emphasis on the use of small satellites. For magnetospheric studies, satellites weighting 100–1000 kg are mainly used. In low Earth orbit (convenient for ionospheric studies) micro- and nanosatellites have dominated in the recent years. The paper formulates scientific objectives for the future micro- and nanosatellites in various orbits, as well as approaches to the assessment of their effectiveness. The paper discusses the common problems of this development field and their possible solutions, both as a whole and for the Russian space program in particular.","PeriodicalId":436954,"journal":{"name":"Rocket-Space Device Engineering and Information Systems","volume":"10 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-12-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"128450519","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
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