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International Journal of Space Science and Engineering最新文献

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Kalman filter and satellite attitude control system analytical design 卡尔曼滤波与卫星姿态控制系统分析设计
IF 0.2 Pub Date : 2020-01-01 DOI: 10.1504/ijspacese.2020.10032070
Y. Kim
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引用次数: 1
On the plasma density variation in the F2 region during geomagnetic storms 磁暴期间F2区等离子体密度的变化
IF 0.2 Pub Date : 2020-01-01 DOI: 10.1504/ijspacese.2020.10032324
R. C. Anamezie, K. Okpala, O. J. Ugonabo
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引用次数: 0
Coherency evaluation of GNSS MBOC pilot and data signal in joint tracking 联合跟踪中GNSS MBOC导频与数据信号的相干性评价
IF 0.2 Pub Date : 2020-01-01 DOI: 10.1504/ijspacese.2020.10032067
Xue Wang, Yao Guo, Zhenghong Zhu, Xiaochun Lu
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引用次数: 1
Conceptual thermal design of a network of solar-powered Boardsat- and CubeSat-based landed spacecraft on Mars 基于太阳能板卫星和立方体卫星的登陆火星航天器网络的概念热设计
IF 0.2 Pub Date : 2020-01-01 DOI: 10.1504/ijspacese.2020.10032472
D. Lee, Regina Lee, J. Moores, T. Young, H. Podmore
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引用次数: 0
Design and analysis of entry, powered descent trajectory envelopes and manifold of landing points 设计和分析进入、动力下降轨迹包络和多种着陆点
IF 0.2 Pub Date : 2020-01-01 DOI: 10.1504/ijspacese.2020.10032477
D. Azimov, Melissa M. Onishi
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引用次数: 0
Impact of geometry sensitive satellites on the navigation performance of ground-based augmented GPS 几何敏感卫星对地基增强型GPS导航性能的影响
IF 0.2 Pub Date : 2020-01-01 DOI: 10.1504/ijspacese.2020.10032069
Dan Zhang, H. Lang, Irfan Sayim
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引用次数: 0
Microgravity, atmosphere sounding, astronomy, technology validation - an overview of suborbital rockets' missions and payloads 微重力,大气探测,天文学,技术验证-亚轨道火箭任务和有效载荷概述
IF 0.2 Pub Date : 2020-01-01 DOI: 10.1504/ijspacese.2020.10032480
R. Puri, T. Noga
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引用次数: 5
Passive vibration suppression of large space truss structures by viscous damping 大型空间桁架结构的粘滞阻尼被动振动抑制
IF 0.2 Pub Date : 2020-01-01 DOI: 10.1504/ijspacese.2020.10032479
Min Luo, Yaobing Wang, Wenbo Luo, Cheng Luo
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引用次数: 2
Satellite formation flying control using an innovative technique subject to electromagnetic acceleration 卫星编队飞行控制采用一种受电磁加速度影响的创新技术
IF 0.2 Pub Date : 2020-01-01 DOI: 10.1504/ijspacese.2020.10032475
K. Khalil, M. E. Awad, Yehia Abdel Aziz, S. Tealib, M. Radwan
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引用次数: 1
Rapid, automated, test, verification and validation for the CubeSats 快速,自动化,测试,验证和确认立方体卫星
IF 0.2 Pub Date : 2019-07-30 DOI: 10.1504/IJSPACESE.2019.101412
Yaseen Zaidi, N. Fitz-Coy, R. V. Zyl
Bringing up of a small-scale mission assurance and engineering workflow is described. The experiences learned in the ZACUBE-1 mission prompted the development of an automated systems engineering platform leading to conformity in system design, test, and verification. The platform implements the methodology of systems engineering by coordinating diverse elements of the lifecycle and by incorporating the tools involved. The phase B/C activities of system modelling, simulations, prototyping, and design may be unified to a compounding effect and raising the level of the system view. The Verification and Validation (V&V) is achieved by integrating a test and measurement facility to the platform. With the platform, we accomplish rapid electrical and functional test and verification of the CubeSat subsystems and thermal validation in 20 °C to +50 °C cycle. The platform is automated by an application software which executes functional and thermal environment tests and provides support for requirements flow, system definition, embedded development, and simulations by integrating real-time target hardware. The platform is exploited in validating an S-band communications subsystem while economizing time and obtaining valuable insight into transmission performance under thermal loading.
提出了一个小规模的任务保证和工程工作流程。在ZACUBE-1任务中获得的经验促进了自动化系统工程平台的发展,从而实现了系统设计、测试和验证的一致性。该平台通过协调生命周期的不同元素和合并所涉及的工具来实现系统工程的方法学。系统建模、模拟、原型和设计的阶段B/C活动可以统一为复合效果,并提高系统视图的级别。验证和确认(V&V)是通过将测试和测量设备集成到平台来实现的。通过该平台,我们完成了CubeSat子系统的快速电气和功能测试和验证,以及20°C至+50°C循环的热验证。该平台由执行功能和热环境测试的应用软件自动化,并通过集成实时目标硬件为需求流、系统定义、嵌入式开发和仿真提供支持。该平台用于验证s波段通信子系统,同时节省时间并获得热负载下传输性能的宝贵见解。
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引用次数: 3
期刊
International Journal of Space Science and Engineering
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