2018 AIAA SPACE and Astronautics Forum and Exposition最新文献

Correction: Alternate Sandwich Panel Core for Space Structures 更正:空间结构的备选夹层板芯

2018 AIAA SPACE and Astronautics Forum and Exposition Pub Date : 2018-09-17 DOI: 10.2514/6.2018-5352.C1

Udit Shah, R. Kapania

引用次数: 0

Correction: Feasibility study for an integrated infrastructure to simulate extraterrestrial environment 更正:模拟地外环境的综合基础设施可行性研究

2018 AIAA SPACE and Astronautics Forum and Exposition Pub Date : 2018-09-17 DOI: 10.2514/6.2018-5155.C1

N. Favaloro, A. Smoraldi, G. Elia, M. Invigorito, Roberto Scigliano

引用次数: 0

Correction: Assessing Cost, Performance and Risk of Human Lunar Exploration Missions Using Robust Portfolio Optimization 修正:利用稳健投资组合优化评估人类月球探测任务的成本、性能和风险

2018 AIAA SPACE and Astronautics Forum and Exposition Pub Date : 2018-09-17 DOI: 10.2514/6.2018-5179.C1

W. O'neill, D. DeLaurentis

引用次数: 0

Correction: Lunar Free Core Nutation detection opens new tasks for the lunar laser ranging and future space missions 修正:月球自由核心章动探测为月球激光测距和未来的太空任务开辟了新的任务

2018 AIAA SPACE and Astronautics Forum and Exposition Pub Date : 2018-09-17 DOI: 10.2514/6.2018-5300.C1

N. Petrova, A. Andreev, Michael Barkin, Y. Nefedyev, A. Zagidullin

引用次数: 0

Correction: Challenges of Power Beaming: Forging production services from the technology development trade space 更正:电力传输的挑战:从技术开发贸易领域锻造生产服务

2018 AIAA SPACE and Astronautics Forum and Exposition Pub Date : 2018-09-17 DOI: 10.2514/6.2018-5368.C1

G. Barnhard, S. Potter

引用次数: 0

Correction: Analysis of the selenophysics parameters using the space missions data 更正:利用空间任务数据分析月球物理参数

2018 AIAA SPACE and Astronautics Forum and Exposition Pub Date : 2018-09-17 DOI: 10.2514/6.2018-5302.C1

A. Andreev, N. Petrova, Y. Nefedyev, N. Demina, E. Kronrod, A. Zagidullin, Sergey V. Demin

引用次数: 0

Correction: Development of a Generic Guidance Navigation & Control System for Small Satellites: Application to HuskySat-1 修正:小型卫星通用制导导航控制系统的开发:在HuskySat-1上的应用

2018 AIAA SPACE and Astronautics Forum and Exposition Pub Date : 2018-09-17 DOI: 10.2514/6.2018-5403.C1

Taylor P. Reynolds, Krish Kaycee, Bijan Barzgaran, Mathias Hudoba de Badyn, Sean Rice, Emma Hansen, A. Adler, Behçet Açikmese, M. Mesbahi

{"title":"Correction: Development of a Generic Guidance Navigation & Control System for Small Satellites: Application to HuskySat-1","authors":"Taylor P. Reynolds, Krish Kaycee, Bijan Barzgaran, Mathias Hudoba de Badyn, Sean Rice, Emma Hansen, A. Adler, Behçet Açikmese, M. Mesbahi","doi":"10.2514/6.2018-5403.C1","DOIUrl":"https://doi.org/10.2514/6.2018-5403.C1","url":null,"abstract":"This paper presents the development of a generic Guidance, Navigation & Control (GNC) system for small satellites at the University of Washington that serves as a testbed for algorithm development and supports small satellite mission design. Our ultimate aim is to advance the capabilities of autonomous satellite operations by demonstrating advanced on-board control and estimation techniques, though the work is equally applicable to earth-imaging, pointing and technology demonstration missions. The work discusses the development of flight software and requisite sensor, actuator and environmental models needed to validate flight software functionality. The first mission application is the HuskySat-1 mission, undertaken by a student-led group at the University of Washington. Primarily a technology demonstration, HuskySat-1 is a 3U CubeSat equipped with a pulsed plasma thruster and a high-frequency communication antenna, equipped with a 3-axis active attitude control subsystem. We demonstrate through software and hardware-based testing that our system supports both scientific payloads. We outline our approach to algorithm development, verification and validation, and briefly hardware-in-the-loop testing.","PeriodicalId":366106,"journal":{"name":"2018 AIAA SPACE and Astronautics Forum and Exposition","volume":"33 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-09-17","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"131532774","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}

引用次数: 1

Correction: High-Integrity TLE Error Models for MEO and GEO Satellites 修正:MEO和GEO卫星的高完整性TLE误差模型

2018 AIAA SPACE and Astronautics Forum and Exposition Pub Date : 2018-09-17 DOI: 10.2514/6.2018-5241.C1

Danielle Racelis, M. Joerger

引用次数: 2

Correction: Analysis of dynamic ephemeris and physical libration of the Moon in order to create a lunar navigational system 修正:分析月球的动态星历和物理振动，以建立月球导航系统

2018 AIAA SPACE and Astronautics Forum and Exposition Pub Date : 2018-09-17 DOI: 10.2514/6.2018-5299.C1

A. Zagidullin, V. Usanin, N. Petrova, A. Andreev, Y. Nefedyev

{"title":"Correction: Analysis of dynamic ephemeris and physical libration of the Moon in order to create a lunar navigational system","authors":"A. Zagidullin, V. Usanin, N. Petrova, A. Andreev, Y. Nefedyev","doi":"10.2514/6.2018-5299.C1","DOIUrl":"https://doi.org/10.2514/6.2018-5299.C1","url":null,"abstract":"Currently, there are a number of projects on robotic and manned exploration of the Moon are being developed. With this purpose, the space agencies pay particular attention to providing coordinate and time support for the upcoming space missions. In particular, Roskosmos is planning to extend GLONASS navigational system to the lunar orbit. Construction of navigational selenocentric systems implies significant development and refinement of the physical libration of the Moon (PLM) numerical theory that defines position of the lunar axes of inertia in relation to the mean ecliptic. In the absence of reliable PLM theory coordinate and time support for the lunar space missions does not have the required accuracy. The present work is mainly concerned with the construction of PLM theory and analysis of its reliability. The authors’ algorithm of building PLM theory and calculating lunar orbit parameters is described. As a result, a numerical PLM theory is developed using DE421 ephemeris. The accuracy of the PLM theory has been assessed by analyzing its residual differences on the basis of comparison with corresponding theories by Rambaux, Williams (Rambaux, N., et al., Rambaux, N., et al.).","PeriodicalId":366106,"journal":{"name":"2018 AIAA SPACE and Astronautics Forum and Exposition","volume":"16 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-09-17","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"133039626","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}

引用次数: 0

Correction: External Verification and Comparison of CubeSat Attitude Determination Filters Using Visual Fiducials 修正:使用视觉基准的立方体卫星姿态确定滤波器的外部验证和比较

2018 AIAA SPACE and Astronautics Forum and Exposition Pub Date : 2018-09-17 DOI: 10.2514/6.2018-5120.C1

J. Liss, G. Elkaim, M. Sorgenfrei, D. Kemp

引用次数: 0