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• W2497319683 abstract "No AccessEngineering NoteTracking Maneuvering Satellite Using Thrust-Fourier-Coefficient Event RepresentationHyun Chul Ko and Daniel J. ScheeresHyun Chul KoUniversity of Colorado at Boulder, Boulder, CO 80309*Graduate Research Assistant, Department of Aerospace Engineering Sciences; .Search for more papers by this author and Daniel J. ScheeresUniversity of Colorado at Boulder, Boulder, CO 80309†University of Colorado Distinguished Professor, A. Richard Sebass Endowed Chair, Department of Aerospace Engineering Sciences, Colorado Center for Astrodynamics Research. Associate Fellow AIAA.Search for more papers by this authorPublished Online:18 Jul 2016https://doi.org/10.2514/1.G000353SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Abbot R. I. and Wallace R. I., “Decision Support in Space Situational Awareness,” Lincoln Laboratory Journal, Vol. 16, No. 2, 2007, pp. 297–335. LLJOEJ 0896-4130 Google Scholar[2] Cloutier J. R., Lin C. F. and Yang C., “Maneuvering Target Tracking via Smoothing and Filtering Through Measurement Concatenation,” Journal of Guidance, Control, and Dynamics, Vol. 16, No. 2, 1993, pp. 377–384. doi:https://doi.org/10.2514/3.21013 JGCODS 0731-5090 LinkGoogle Scholar[3] Goff G. M., Black J. T. and Beck J. A., “Tracking Maneuvering Spacecraft with Filter-Through Approaches Using Interacting Multiple Models,” Acta Astronautica, Vol. 114, Sept.–Oct. 2015, pp. 152–163. doi:https://doi.org/10.1016/j.actaastro.2015.05.009 AASTCF 0094-5765 CrossrefGoogle Scholar[4] Spingarn K. and Weidemann H. L., “Linear Regression Filtering and Prediction for Tracking Maneuvering Aircraft Vehicles,” IEEE Transactions on Aerospace and Electronics System, Vol. AES-8, No. 6, 1972, pp. 800–810. doi:https://doi.org/10.1109/TAES.1972.309612 CrossrefGoogle Scholar[5] Yun J. and Ryoo C. K., “Missile Guidance Law Estimation Using Modified Interactive Multiple Model Filter,” Journal of Guidance, Control, and Dynamics, Vol. 37, No. 2, 2014, pp. 484–496. doi:https://doi.org/10.2514/1.61327 JGCODS 0731-5090 LinkGoogle Scholar[6] Li X. R. and Jilkov V. P., “A Survey of Maneuvering Target Tracking–Part IV: Decision-Based Methods,” Proceedings of SPIE Conference on Signal and Data Processing of Small Targets, Vol. 4728, SPIE Publ., Bellingham, Washington, D.C., April 2002, pp. 511–534. doi:https://doi.org/10.1117/12.478535 Google Scholar[7] Schlee F. H., Standish C. J. and Toda N. F., “Divergence in the Kalman Filter,” AIAA Journal, Vol. 5, No. 6, 1967, pp. 1114–1120. doi:https://doi.org/10.2514/3.4146 AIAJAH 0001-1452 LinkGoogle Scholar[8] Tarn T. J. and Zaborsky J., “A Practical Non-Diverging Filter,” AIAA Journal, Vol. 8, No. 6, 1970, 1127–1133. doi:https://doi.org/10.2514/3.5842 AIAJAH 0001-1452 LinkGoogle Scholar[9] Jazwinski A. H., Stochastic Processes and Filter Theory, Academic Press, New York, 1970, pp. 292–322, Chap. 8. Google Scholar[10] Hampton R. L. T. and Cooke J. R., “Unsupervised Tracking of Maneuvering Vehicles,” IEEE Transactions on Aerospace Electronic Systems, Vol. AES-2, No. 2, 1973, pp. 197–207. doi:https://doi.org/10.1109/TAES.1973.309767 CrossrefGoogle Scholar[11] Maybeck P. S. and Hentz K. P., “Investigation of Moving-Bank Multiple Model Adaptive Algorithms,” Journal of Guidance, Control, and Dynamics, Vol. 10, No. 1, 1987, pp. 90–96. doi:https://doi.org/10.2514/3.20185 JGCODS 0731-5090 LinkGoogle Scholar[12] Blom H. A. P. and Bar-Shalom Y., “The Interacting Multiple Model Algorithm for Systems with Jump-Linear Smoothing Application,” IEEE Transactions on Automatic Control, Vol. 33, No. 8, 1988, pp. 780–783. doi:https://doi.org/10.1109/9.1299 CrossrefGoogle Scholar[13] Munir A. and Atherton D. P., “Adaptive Interacting Multiple Model Algorithm for Tracking a Maneuvering Target,” IEE Proceedings of Radar, Sonar, and Navigation, Vol. 142, No. 1, 1995, pp. 11–17. doi:https://doi.org/10.1049/ip-rsn:19951528 CrossrefGoogle Scholar[14] Lee S. and Hwang I., “Interacting Multiple Model Estimation for Spacecraft Maneuver Detection and Characterization,” Proceedings of the AIAA Guidance, Navigation, and Control Conference, AIAA Paper 2015-1333, Jan. 2015. LinkGoogle Scholar[15] Goff G. M., Black J. T. and Beck J. A., “Orbit Estimation of a Continuously Thrusting Spacecraft Using Variable Dimension Filters,” Journal of Guidance, Control, and Dynamics, Vol. 38, No. 12, 2015, pp. 2407–2420. doi:https://doi.org/10.2514/1.G001091 JGCODS 0731-5090 LinkGoogle Scholar[16] Singer R. A., “Estimating Optimal Tracking Filter Performance for Manned Maneuvering Target,” IEEE Transactions on Aerospace Electronic Systems, Vol. AES-6, No. 4, 1970, pp. 473–483. doi:https://doi.org/10.1109/TAES.1970.310128 CrossrefGoogle Scholar[17] Jazwinski A. H., “Adaptive Filtering,” Automatica, Vol. 5, No. 4, 1969, pp. 475–485. doi:https://doi.org/10.1016/0005-1098(69)90109-5 ATCAA9 0005-1098 CrossrefGoogle Scholar[18] Chen G. and Chui C. K., “A Modified Adaptive Kalman Filter for Real-Time Applications,” IEEE Transactions on Aerospace Electronic Systems, Vol. 27, No. 1, 1991, pp. 149–154. doi:https://doi.org/10.1109/7.68157 CrossrefGoogle Scholar[19] Belanger P. R., “Estimation of Noise Covariance Matrices for a Linear Time-Varying Stochastic Process,” Automatica, Vol. 10, No. 3, 1974, pp. 267–275. doi:https://doi.org/10.1016/0005-1098(74)90037-5 ATCAA9 0005-1098 CrossrefGoogle Scholar[20] Chan Y. T., Hu G. C. and Plant J. B., “A Kalman Filter Based Tracking Scheme with Input Estimation,” IEEE Transactions on Aerospace and Electronics System, Vol. AES-15, No. 2, 1979, pp. 237–244. doi:https://doi.org/10.1109/TAES.1979.308710 CrossrefGoogle Scholar[21] Whang I. H., Lee J. and Sung T., “Modified Input Estimation Technique Using Pseudoresidual,” IEEE Transactions on Aerospace and Electronics System, Vol. 30, No. 1, 1994, pp. 220–228. doi:https://doi.org/10.1109/7.250422 CrossrefGoogle Scholar[22] Bogler P. L., “Tracking a Maneuvering Target Using Input Estimation,” IEEE Transactions on Aerospace and Electronics System, Vol. AES-23, No. 3, 1987, pp. 298–310. doi:https://doi.org/10.1109/TAES.1987.310826 CrossrefGoogle Scholar[23] Lee H. and Tahk M. J., “Generalized Input-Estimation Technique for Tracking Maneuvering Targets,” IEEE Transactions on Aerospace and Electronics System, Vol. AES-35, No. 4, 1999, pp. 1388–1402. Google Scholar[24] Bar-Shalom Y. and Birmiwal K., “Variable Dimension Filter for Maneuvering Target Tracking,” IEEE Transactions on Aerospace and Electronics System, Vol. AES-18, No. 5, 1982, pp. 621–629. doi:https://doi.org/10.1109/TAES.1982.309274 CrossrefGoogle Scholar[25] Cloutier J. R., Lin C. F. and Yang C., “Enhanced Variable Dimension Filter for Maneuvering Target Tracking,” IEEE Transactions on Aerospace and Electronics System, Vol. 29, No. 3, 1993, pp. 786–797. doi:https://doi.org/10.1109/7.220930 CrossrefGoogle Scholar[26] Friedland B., “Treatment of Bias in Recursive Filtering,” IEEE Transactions on Automatic Control, Vol. 14, No. 4, 1969, pp. 359–367. doi:https://doi.org/10.1109/TAC.1969.1099223 IETAA9 0018-9286 CrossrefGoogle Scholar[27] Hu X., Hu X. and Huang Y., “A Nonlinear Variable Dimension Estimator for Maneuvering Spacecraft Tracking via the Unscented Kalman Filter,” IEEE International Conference on Information and Automation, IEEE Publ., Piscataway, NJ, June 2008, pp. 226–231. Google Scholar[28] Ko H. C. and Scheeres D. J., “Event Representation Based Orbit Determination Across Unknown Space Events,” Journal of Guidance, Control, and Dynamics, Vol. 38, No. 2351, 2015, pp. 2351–2365. doi:https://doi.org/10.2514/1.G001050 JGCODS 0731-5090 LinkGoogle Scholar[29] Ko H. C. and Scheeres D. J., “Essential Thrust-Fourier-Coefficient Set of Averaged Gauss Equations for Orbital Mechanics,” Journal of Guidance, Control, and Dynamics, Vol. 37, No. 4, 2014, pp. 1236–1249. doi:https://doi.org/10.2514/1.62407 JGCODS 0731-5090 LinkGoogle Scholar[30] Ko H. C. and Scheeres D. J., “Orbit Determination and Maneuver Detection Using Event Representation with Thrust-Fourier-Coefficients,” Proceedings of the Advanced Maui Optical and Space Surveillance Technologies Conference, Maui Economics Development Board, Maui, HI, Sep. 2015. Google Scholar[31] Scheeres D. J. and Holzinger M. J., “The Control Distance Metric and Constraints on Maneuvering Satellites,” 15th International Conference on Information Fusion (FUSION) 2012, IEEE, Singapore, July 2012, pp. 2035–2042. Google Scholar[32] Haberman R., Applied Partial Differential Equations with Fourier Series and Boundary Value Problems, 4th ed., Pearson Prentice-Hall, Upper Saddle River, NJ, 2004, pp. 89–92. Google Scholar[33] Hudson J. S. and Scheeres D. J., “Reduction of Low-Thrust Continuous Controls for Trajectory Dynamics,” Journal of Guidance, Control, and Dynamics, Vol. 32, No. 3, 2009, pp. 780–787. doi:https://doi.org/10.2514/1.40619 JGCODS 0731-5090 LinkGoogle Scholar[34] Ko H. C. and Scheeres D. J., “Maneuver Detection with Event Representation Using Thrust-Fourier-Coefficients,” 2015 AAS/AIAA Astrodynamics Specialist Conference, AAS/AIAA Paper 2015-631, Aug. 2015. Google Scholar Previous article Next article" @default.
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