Monocamera-Based Solar Radiation Pressure Estimation for Small-Body Rendezvous Missions

No AccessEngineering NoteMonocamera-Based Solar Radiation Pressure Estimation for Small-Body Rendezvous MissionsS. Delchambre, T. Ziegler, C. P. Diego Trigueros, A. Falke, U. Johann and K. JanschekS. DelchambreAirbus Defence and Space GmbH, 88090 Immenstaad, Germany*AOCS/GNC and FD Engineer, AOCS/GNC and Flight Dynamics Department; .Search for more papers by this author, T. ZieglerAirbus Defence and Space GmbH, 88090 Immenstaad, Germany†AOCS and GNC Architect, AOCS/GNC and Flight Dynamics Department; .Search for more papers by this author, C. P. Diego TriguerosCranfield University, Cranfield MK43 0AL, England, United Kingdom‡Aerospace Master Student; .Search for more papers by this author, A. FalkeAirbus Defence and Space GmbH, 88090 Immenstaad, Germany§Space Systems Engineer, Project Management and Small Body Missions Programmatics; Advanced Projects Department; .Search for more papers by this author, U. JohannAirbus Defence and Space GmbH, 88090 Immenstaad, Germany¶Space Senior Export Engineer, Future Programmes Department; .Search for more papers by this author and K. JanschekTechnical University Dresden, 01187 Dresden, Germany**Univ.-Prof. Dr. Techn., Institute of Automation, Faculty of Electrical and Computer Engineering; .Search for more papers by this authorPublished Online:7 May 2018https://doi.org/10.2514/1.G003416SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Vallado D. A., Fundamentals of Astrodynamics and Applications, 2nd ed., Microcosm Press Jointly with Kluwer Academic Publ., Torrance, CA, 2001, p. 546, Sec. 8.6.4. Google Scholar[2] Kuninaka H. and Kawaguchi J., “Lessons Learned from Round Trip of Hayabusa Asteroid Explorer in Deep Space,” Proceedings of the IEEE Aerospace Conference, IEEE Publ., Piscataway, NJ, 2011, pp. 1–8. doi:https://doi.org/10.1109/AERO.2011.5747599 Google Scholar[3] Antreasian P. G., Moreau M., Jackman C., Williams K., Page B. and Leonard J. M., “OSIRIS-REx Orbit Determination Covariance Studies at Bennu,” Advances in the Astronautical Sciences Guidance, Navigation, and Control, AAS Paper 16-101, Vol. 157, 2016. Google Scholar[4] McMahon J. W. and Scheeres D. J., “New Solar Radiation Pressure Force Model for Navigation,” Journal of Guidance, Control, and Dynamics, Vol. 33, No. 5, 2010, pp. 1418–1428. doi:https://doi.org/10.2514/1.48434 JGCODS 0731-5090 LinkGoogle Scholar[5] Žižka J. and Vokrouhlický D., “Solar Radiation Pressure on (99942) Apophis,” Icarus, Vol. 211, No. 1, 2011, pp. 511–518. doi:https://doi.org/10.1016/j.icarus.2010.08.011 ICRSA5 0019-1035 CrossrefGoogle Scholar[6] Yamaguchi T., Mimasu Y., Tsuda Y., Funase R., Sawada H., Mori O., Morimoto M. Y., Takeuchi H. and Yoshikawa M., “Trajectory Analysis of Small Solar Sail Demonstration Spacecraft IKAROS Considering the Uncertainty of Solar Radiation Pressure,” Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, Vol. 8, No. ists27, 2010, pp. Pd_37–Pd_43. doi:https://doi.org/10.2322/tastj.8.Pd_37 CrossrefGoogle Scholar[7] Colombo O. L., “The Dynamics of Global Positioning System Orbits and the Determination of Precise Ephemerides,” Journal of Geophysical Research, Vol. 94, July 1989, pp. 9167–9182. doi:https://doi.org/10.1029/JB094iB07p09167 JGREA2 0148-0227 CrossrefGoogle Scholar[8] Liu J., Gu D., Ju B., Shen Z., Lai Y. and Yi D., “A New Empirical Solar Radiation Pressure Model for BeiDou GEO Satellites,” Advances in Space Research, Vol. 57, No. 1, 2016, pp. 234–244. doi:https://doi.org/10.1016/j.asr.2015.10.043 ASRSDW 0273-1177 CrossrefGoogle Scholar[9] Ala-Luhtala J., Seppänen M. and Piche R., “An Empirical Solar Radiation Pressure Model for Autonomous GNSS Orbit Prediction,” Proceedings of the 2012 IEEE/ION Position, Location and Navigation Symposium, 2012, pp. 568–575. CrossrefGoogle Scholar[10] Yamaguchi T., Mimasu Y., Tsuda Y. and Yoshikawa M., “Hybrid Estimation of Solar Radiation Pressure for a Spinning Solar Sail Spacecraft,” Journal of Spacecraft and Rockets, Vol. 51, No. 1, 2014, pp. 381–384. doi:https://doi.org/10.2514/1.A32387 JSCRAG 0022-4650 LinkGoogle Scholar[11] Bruinsma S., Loyer S., Lemoine J. M., Perosanz F. and Tamagnan D., “The Impact of Accelerometry on CHAMP Orbit Determination,” Journal of Geodesy, Vol. 77, Nos. 1–2, 2003, pp. 86–93. doi:https://doi.org/10.1007/s00190-002-0304-3 JOGEF8 0949-7714 CrossrefGoogle Scholar[12] Flury J., Bettadpur S. and Tapley B. D., “Precise Accelerometry On-Board the GRACE Gravity Field Satellite Mission,” Advances in Space Research, Vol. 42, No. 8, 2008, pp. 1414–1423. doi:https://doi.org/10.1016/j.asr.2008.05.004 ASRSDW 0273-1177 CrossrefGoogle Scholar[13] Iafolla V., Fiorenza E., Lefevre C., Lucchesi D. M., Lucente M., Magnafico C., Peron A. and Santoli F., “The BepiColombo ISA Accelerometer: Ready for Launch,” Proceedings of 2016 IEEE Metrology for Aerospace Conference, IEEE Publ., Piscataway, NJ, 2016. doi:https://doi.org/10.1109/MetroAeroSpace.2016.7573273 Google Scholar[14] Pardo de Santayana R. and Lauer M., “Optical Measurements for Rosetta Navigation near the Comet,” Proceedings of International Symposium for Space Flight Dynamics, DLR/GSOC Paper 062, 2015. Google Scholar[15] Lorenz D. A., Olds R., May A., Mario C., Perry M. E., Palmer E. E. and Daly M., “Lessons Learned from OSIRIS-REx Autonomous Navigation Using Natural Feature Tracking,” 38th IEEE Aerospace Conference, IEEE Publ., Piscataway, NJ, 2017. doi:https://doi.org/10.1109/AERO.2017.7943684 Google Scholar[16] Scheeres D. J., Orbital Motion in Strongly Perturbed Environments: Applications to Asteroid, Comet and Planetary Satellite Orbiters, Springer, New York, 2012, p. 243, Chap. 11. CrossrefGoogle Scholar[17] Fujiwra A., Kawaguchi J., Yeomans D. K., Abe M., Mukai T., Okada T., Saito J., Yano H., Yoshikawa M., Scheeres D. J., Barnouin O., Chang A. F., Demura H., Gaskell R. W., Hirata N., Ikeda H., Kominato T., Miyamoto H., Nakamura A. M., Nakamura R., Sasaki S. and Uesugi K., “The Rubble-Pile Asteroid Itokawa as Observed by Hayabusa,” Science, Vol. 312, No. 5778, 2006, pp. 1330–1334. doi:https://doi.org/10.1126/science.1125841 SCIEAS 0036-8075 CrossrefGoogle Scholar[18] Delchambre S., Ziegler T., Johann U., Falke A. and Janschek K. J., “Landmark Based Pose Estimation for Autonomous Inertial Hovering Around Small Solar System Bodies,” 10th International ESA GNC Conference on Guidance, Navigation & Control Systems, ESA, Salzburg, 2017. Google Scholar[19] Delchambre S., Martin M., Harbulot Q., Ziegler T., Falke A., Johann U. and Janschek K. J., “Near-Inertial Hovering Optical Navigation at the Close Proximity of Very Small Asteroids,” 5th Planetary Defence Conference, Paper IAA-PDC-17-05-P20, 2017. Google Scholar[20] Hartley R. I. and Zisserman A., “Multiple View Geometry in Computer Vision,” Camera Models—Finite Cameras, 2nd ed., Cambridge Univ. Press, Cambridge, U.K., 2004, pp. 153–158. CrossrefGoogle Scholar[21] Antreasian P. G. and Rosborough G. W., “Prediction of Radiant Energy Forces on the TOPEX/Poseidon Spacecraft,” Journal of Spacecraft and Rockets, Vol. 29, No. 1, Jan.–Feb. 1992, pp. 81–90. doi:https://doi.org/10.2514/3.26317 JSCRAG 0022-4650 LinkGoogle Scholar[22] Qui J., Goode P. R., Palle E., Yurchyshun V., Hickey J., Rodriguey Montanes P., Chu M.-C., Kolbe E., Brown C. T. and Koonin S. E., “Earthshine and the Earth’s Albedo: 1. Earthshine Observations and Measurements of the Lunar Phase Function for Accurate Measurements of the Earth’s Bond Albedo,” Journal of Geophysical Research, Vol. 108, No. D22, p. 4709. doi:https://doi.org/10.1029/2003JD003610 JGREA2 0148-0227 Google Scholar[23] Bottke W. F., Vokrouhlický D., Rubincam D. P. and Nesvorný D., “The Yarkovsky and YORP Effects: Implications for Asteroid Dynamics,” Annual Review of Earth and Planetary Sciences, Vol. 34, No. 1, 2006, pp. 157–191. doi:https://doi.org/10.1146/annurev.earth.34.031405.125154 AREPCI 0084-6597 CrossrefGoogle Scholar[24] Shor V. A., Chernetenko Y. A., Kochetova O. M. and Yheleynov N. B., “On the Impact of the Yarkovsky Effect on Apophis’ Orbit,” Astronomicheskii Vestnik, Vol. 46, No. 2, 2012, pp. 131–142. doi:https://doi.org/10.1134/S0038094612010078 ASVEA7 0320-930X Google Scholar[25] Kirchgraber U. R. S., “A Problem of Orbital Dynamics, Which Is Separable in KS-Variables,” Celestial Mechanics, Vol. 4, Nos. 3–4, 1971, pp. 340–347. doi:https://doi.org/10.1007/BF01231396 CLMCAV 0008-8714 CrossrefGoogle Scholar[26] Greene W. H., “Econometric Analysis,” The Least Squares Estimator, 5th ed., Pearson Education Inc., Upper Saddle River, NJ, 2003, p. 98. Google Scholar Previous article Next article FiguresReferencesRelatedDetails What's Popular Volume 41, Number 8August 2018 CrossmarkInformationCopyright © 2018 by the American Institute of Aeronautics and Astronautics, Inc. 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. TopicsAsteroidsAstronomyCelestial MechanicsPlanetary Science and ExplorationPlanetsSolar PhysicsSpace Exploration and TechnologySpace MissionsSpace Science and Technology KeywordsSolar RadiationAlbedoOrbit DeterminationAsteroidsGNSSSolar SailAccelerometerGPSPropellantGravity Recovery and Climate ExperimentAcknowledgmentsThe results described here have been made possible with support from Airbus Defence and Space R&D department and the NEOShield-2 project, which has received funding from the European Union’s Horizon 2020 research and innovation program under Grant Agreement No. 640351.PDF Received30 October 2017Accepted22 March 2018Published online7 May 2018