Magnetometer-Based Attitude Determination for Deployed Spin-Stabilized Spacecraft
2017; American Institute of Aeronautics and Astronautics; Volume: 40; Issue: 11 Linguagem: Inglês
10.2514/1.g002591
ISSN1533-3884
AutoresT.M. Roberts, K. A. Lynch, R. Clayton, Michael E. Disbrow, C. Hansen,
Tópico(s)GNSS positioning and interference
ResumoNo AccessEngineering NoteMagnetometer-Based Attitude Determination for Deployed Spin-Stabilized SpacecraftT. Maximillian Roberts, Kristina A. Lynch, Robert E. Clayton, Michael E. Disbrow and Christopher J. HansenT. Maximillian RobertsDartmouth College, Hanover, New Hampshire 03755*Postdoctoral Researcher, Department of Physics and Astronomy, Wilder Laboratory.Search for more papers by this author, Kristina A. LynchDartmouth College, Hanover, New Hampshire 03755†Professor, Department of Physics and Astronomy, Wilder Laboratory.Search for more papers by this author, Robert E. ClaytonDartmouth College, Hanover, New Hampshire 03755‡Graduate Student, Department of Physics and Astronomy, Wilder Laboratory.Search for more papers by this author, Michael E. DisbrowNASA Wallops Flight Facility, Wallops Island, Virginia 23337§Flight Performance Engineer, NASA Sounding Rocket Operations.Search for more papers by this author and Christopher J. HansenUniversity of Washington, Seattle, Washington 98105¶Research Scientist, William E. Boeing Department of Aeronautics and Astronautics, Box 352400.Search for more papers by this authorPublished Online:26 Jun 2017https://doi.org/10.2514/1.G002591SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Roberts T. M., “A Low-Resource, Deployed Spacecraft for Multipoint Measurement of Ionospheric Plasma,” Review of Scientific Instruments (submitted for publication). RSINAK 0034-6748 Google Scholar[2] Knudsen W. C., “Evaluation and Demonstration of the Use of Retarding Potential Analyzers for Measuring Several Ionospheric Quantities,” Journal of Geophysical Research: Space Physics (1978–2012), Vol. 71, No. 19, Oct. 1966, pp. 4669–4678. doi:https://doi.org/10.1029/JZ071i019p04669 CrossrefGoogle Scholar[3] Fanelli L., Noel S., Earle G. D., Fish C., Davidson R. L., Robertson R. 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R. and Horak P., “Including Sheath Effects in the Interpretation of Planar Retarding Potential Analyzer’s Low-Energy Ion Data,” Review of Scientific Instruments, Vol. 87, No. 4, April 2016, Paper 043504. doi:https://doi.org/10.1063/1.4944416 RSINAK 0034-6748 CrossrefGoogle Scholar[6] Fisher L., “Overcoming and Utilizing Plasma Sheaths for Low Energy Plasma Analysis,” Ph.D. Dissertation, Dartmouth College, Hanover, NH, May 2016, pp. 1–149. Google Scholar[7] “Ultra-Compact High-Performance eCompass Module: 3-D Accelerometer and 3-D Magnetometer,” LSM303-D Datasheet, STMicroelectronics, Geneva, Nov. 2013, www.st.com/resource/en/datasheet/lsm303d.pdf [retrieved 2017]. Google Scholar[8] Lerner G. M. and Shuster M. D., “In-Flight Magnetometer Calibration and Attitude Determination for Near-Earth Spacecraft,” Journal of Guidance, Control, and Dynamics, Vol. 4, No. 5, 1981, pp. 518–522. doi:https://doi.org/10.2514/3.56101 JGCODS 0731-5090 LinkGoogle Scholar[9] Vasconcelos J. F., Elkaim G., Silvestre C., Oliveira P. and Cardeira B., “Geometric Approach to Strapdown Magnetometer Calibration in Sensor Frame,” IEEE Transactions on Aerospace and Electronic Systems, Vol. 47, No. 2, April 2011, pp. 1293–1306. doi:https://doi.org/10.1109/TAES.2011.5751259 IEARAX 0018-9251 CrossrefGoogle Scholar[10] Newville M., Stensitzki T., Allen D. B. and Ingargiola A., “LMFIT: Non-Linear Least-Square Minimization and Curve-Fitting for Python,” Zenodo [online database], European Organization for Nuclear Research (CERN), Geneva, Sept. 2014. doi:https://doi.org/10.5281/zenodo.11813 Google Scholar Previous article Next article FiguresReferencesRelatedDetailsCited bySpatiotemporal Limitations of Data‐Driven Modeling: An ISINGLASS Case Study30 August 2022 | Journal of Geophysical Research: Space Physics, Vol. 127, No. 9Applications of a Single-Vector Inertial Aiding Scheme for 3U CubeSatsKail Laughlin, Demoz Gebre-Egziabher and Vibhor L. 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All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the ISSN 0731-5090 (print) or 1533-3884 (online) to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsEarth SciencesElectromagnetismGeneral PhysicsGeophysicsMagnetismMagnetometersSpace Systems and VehiclesSpacecrafts KeywordsThree Axis MagnetometerRigid SpacecraftAttitude Control SystemSounding RocketsGyroscopesGPSGeomagnetic FieldNASA Wallops Flight FacilityAccelerometerCAD SoftwareAcknowledgmentsWe acknowledge sounding rocket support from NASA/Low Cost Access to Space (NNX14AH07G) and research funding from NASA/NH Experimental Program to Stimulate Competitive Research (NNX15AK51A).PDF Received6 November 2016Accepted25 April 2017Published online26 June 2017
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