2021年最新SCI期刊影响因子查询系统
JOURNAL OF THE ASTRONAUTICAL SCIENCES 期刊详细信息
基本信息
期刊名称 | JOURNAL OF THE ASTRONAUTICAL SCIENCES JOURNAL OF THE ASTRONAUTICAL SCIENCES |
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期刊ISSN | 0021-9142 |
期刊官方网站 | http://link.springer.com/journal/40295 |
是否OA | 否 |
出版商 | Springer US |
出版周期 | Quarterly |
始发年份 | |
年文章数 | 21 |
最新影响因子 | 1.56(2021) |
中科院SCI期刊分区
大类学科 | 小类学科 | Top | 综述 |
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工程技术4区 | ENGINEERING, AEROSPACE 工程:宇航3区 | 否 | 否 |
CiteScore
CiteScore排名 | CiteScore | SJR | SNIP | ||
---|---|---|---|---|---|
学科 | 排名 | 百分位 | 1.64 | 0.701 | 1.646 |
Engineering Aerospace Engineering |
38 / 119 | 68% |
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Earth and Planetary Sciences Space and Planetary Science |
47 / 86 | 45% |
补充信息
自引率 | 6.90% |
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H-index | 43 |
SCI收录状况 |
Science Citation Index Expanded |
官方审稿时间 | Submission to first decision 213 days |
网友分享审稿时间 | 数据统计中,敬请期待。 |
PubMed Central (PML) | http://www.ncbi.nlm.nih.gov/nlmcatalog?term=0021-9142%5BISSN%5D |
投稿指南
期刊投稿网址 | https://www.editorialmanager.com/jass/default.aspx |
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收稿范围 | The Journal of the Astronautical Sciences was founded in 1954 as an archival publication devoted to the science and technology of astronautics. Articles are published which present significant new results, important insights, or state of the art surveys in all areas of astrodynamics, celestial mechanics, atmospheric flight mechanics, navigation and guidance, and space related sciences. Authors are encouraged to submit papers on attitude dynamics, orbit determination, trajectory optimization, space missions analysis, numerical methods, maneuvering flight vehicles, dynamics and control of large flexible space structures, and space science related to new astronautical systems and their applications. Table of Contents for Volume 59, Issues 1-2: Coming Soon! Majji, Junkins, and Turner Measurement Model Nonlinearity in Estimation of Dynamical Systems Elipe, Lanchares and Pascual Resonances and the Stability of Stationary Points Around a Central Body Ferrer and Lara On Roto-Translatory Motion, Reductions and Radial Intermediaries Scheeres, de Gosson, and Maruskin Applications of Symplectic Topology to Orbit Uncertainty and Space craft Navigation Juang and Wang Further Studies on Singular Value Method for Star Pattern Recognition and Attitude Determination Satak, Davis, Doebbler and Hurtado Two Impulse Reorientation of Spinning Axisymmetric Body: Single Axis Thrust Lee and Juang Nonlinear System Identification – A continuous-Time Bilinear State Space Approach Phan and Čelk A Superspace Method for Discrete-Time Bilinear Model Identification by Interaction Matrices Shi and Longman The Influence on Stability Robustness of Compromising on the Zero Tracking Error Requirement in Repetitive Control Turner and Elgohary Generalized Frequency Domain State-Space Models for analyzing Flexible Rotating Spacecraft Kaplinger, Wie, and Dearborn Earth-Impact and Analysis of a Near-Earth Object Fragmented and Dispersed by nuclear Subsurface Explosions Roscoe, Vadali, and Alfriend Design of Satellite Formations in Orbits of High Eccentricity with Performance Constraints Specified over a Region of Interest Schaub and Moorer Geosynchronous Large Debris Reorbiter: Challenges and Prospects McLaughlin, Lechtenberg, Fattig, and Krishna Estimating Density Using Precision Satellite Orbits from Multiple Satellites Yan and Gong Feedback control for Formation Flying Maintenance Using State Transition Matrix Russell and Lantoine Optimal Control of Relative Motion in Arbitrary Fields: Application at Deimos Sengupta Elliptic Rendezvous in the Chaser Satellite Frame Huang Optimal Multi-Impulse Orbit Transfer using Nonlinear Relative Motion Dynamics Hill, Sabol, and Alfriend Comparison of Covariance Track Association Approaches Using Simulated Data Seidelmann Space Surveillance – U.S., Russia, and China Carpenter and Markley Sequential Probability Ratio Test for Collision Avoidance Maneuver Decisions Fujimoto and Scheeres Correlation of Optical Observations of Earth-Orbiting Objects by Means of Probability Distributions Gaebler, Hur-Diaz, and Carpenter Comparison of Sigma-Point and Extended Kalman Filters on a Realistic Orbit Determination Scenario Horwood, Aragon, and Poore Adaptive Gaussian Sum Filters for Space Surveillance Tracking Bai and Junkins Modified Chebyshev-Picard Iteration Methods for Solution of Initial Value Problems Wright LS GEO IOD Hoots and Sorge Satellite Breakup Parameter Determination |
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