谷歌浏览器插件
订阅小程序
在清言上使用

Computationally Efficient Attitude Estimation with Extended H2 Filtering

Journal of guidance, control, and dynamics(2021)

引用 4|浏览4
暂无评分
摘要
No AccessEngineering NotesComputationally Efficient Attitude Estimation with Extended H2 FilteringSunsoo Kim, Vaishnav Tadiparthi and Raktim BhattacharyaSunsoo KimTexas A&M University, College Station, Texas 77840*Graduate Student, Electrical and Computer Engineering. Student Member AIAA.Search for more papers by this author, Vaishnav TadiparthiTexas A&M University, College Station, Texas 77840†Graduate Student, Aerospace Engineering. Student Member AIAA.Search for more papers by this author and Raktim BhattacharyaTexas A&M University, College Station, Texas 77840‡Associate Professor, Aerospace Engineering. Associate Fellow AIAA.Search for more papers by this authorPublished Online:28 Oct 2020https://doi.org/10.2514/1.G005140SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Eure K. W., Quach C. C., Vazquez S. L., Hogge E. F. and Hill B. L., “An Application of UAV Attitude Estimation Using a Low-Cost Inertial Navigation System,” NASA/TM–2013-218144, 2013. Google Scholar[2] Gebre-Egziabher D., Hayward R. and Powell J., “Design of Multi-Sensor Attitude Determination Systems,” IEEE Transactions on Aerospace and Electronic Systems, Vol. 40, No. 2, 2004, pp. 627–649. https://doi.org/10.1109/TAES.2004.1310010 CrossrefGoogle Scholar[3] Kada B., Munawar K., Shaikh M., Hussaini M. and Al-Saggaf U., “UAV Attitude Estimation Using Nonlinear Filtering and Low-Cost Mems Sensors,” IFAC-PapersOnLine, Vol. 49, No. 21, 2016, pp. 521–528. https://doi.org/10.1016/j.ifacol.2016.10.655 CrossrefGoogle Scholar[4] Weibel D., Lawrence D. and Palo S., “Small Unmanned Aerial System Attitude Estimation for Flight in Wind,” Journal of Guidance, Control, and Dynamics, Vol. 38, No. 7, 2015, pp. 1300–1305. https://doi.org/10.2514/1.G000888 LinkGoogle Scholar[5] Crassidis J. L., Markley F. L. and Cheng Y., “Survey of Nonlinear Attitude Estimation Methods,” Journal of Guidance, Control, and Dynamics, Vol. 30, No. 1, 2007, pp. 12–28. https://doi.org/10.2514/1.22452 LinkGoogle Scholar[6] Ludwig S. A. and Burnham K. D., “Comparison of Euler Estimate Using Extended Kalman Filter, Madgwick and Mahony on Quadcopter Flight Data,” 2018 International Conference on Unmanned Aircraft Systems (ICUAS), Inst. of Electrical and Electronics Engineers, New York, 2018. https://doi.org/10.1109/icuas.2018.8453465 Google Scholar[7] Teague H., “Comparison of Attitude Estimation Techniques for Low-Cost Unmanned Aerial Vehicles,” 2016. Google Scholar[8] Trawny N. and Roumeliotis S. I., “Indirect Kalman Filter for 3D Attitude Estimation,” Dept. of Computer Science & Engineering, Univ. of Minnesota TR 2005-002, Vol. 2, 2005. Google Scholar[9] Ko N., Jeong S. and Bae Y., “Sine Rotation Vector Method for Attitude Estimation of an Underwater Robot,” Sensors, Vol. 16, No. 8, 2016, p. 1213. https://doi.org/10.3390/s16081213 CrossrefGoogle Scholar[10] Jing X., Cui J., He H., Zhang B., Ding D. and Yang Y., “Attitude Estimation for UAV Using Extended Kalman Filter,” 2017 29th Chinese Control and Decision Conference (CCDC), Inst. of Electrical and Electronics Engineers, New York, 2017. https://doi.org/10.1109/ccdc.2017.7979077 Google Scholar[11] Madgwick S., “An Efficient Orientation Filter for Inertial and Inertial/Magnetic Sensor Arrays,” Vol. 25, Report x-io and Univ. of Bristol, Bristol, England, U.K., 2010, pp. 113–118. Google Scholar[12] Simon D., Optimal State Estimation, Wiley, New York, 2006. https://doi.org/10.1002/0470045345 CrossrefGoogle Scholar[13] Kim S., Tadiparthi V. and Bhattacharya R., “Nonlinear Attitude Estimation for Small UAVs with Low Power Microprocessors,” 2020 American Control Conference (ACC), Inst. of Electrical and Electronics Engineers, New York, 2020. https://doi.org/10.23919/acc45564.2020.9147415 Google Scholar[14] Choukroun D., Cooper L. and Berman N., “Spacecraft Attitude Estimation and Gyro Calibration via Stochastic H ∞ Filtering,” Advances in Aerospace Guidance, Navigation and Control, Springer, Berlin, 2011, pp. 397–415. https://doi.org/10.1007/978-3-642-19817-5_31 Google Scholar[15] Goldstein H., Poole C. and Safko J., “Classical Mechanics,” American Journal of Physics, Vol. 70, No. 7, 2002, pp. 782–783. https://doi.org/10.1119/1.1484149 Google Scholar[16] Carrillo L. R. G., López A. E. D., Lozano R. and Pégard C., “Modeling the Quad-Rotor Mini-Rotorcraft,” Advances in Industrial Control, Springer, London, 2013, pp. 23–34. https://doi.org/10.1007/978-1-4471-4399-4_2 Google Scholar[17] Allen R. and Chang D., “Performance Testing of the Systron Donner Quartz Gyro,” JPL Engineering Memorandum, EM, 1993, pp. 343–1297. Google Scholar[18] El-Sheimy N., Hou H. and Niu X., “Analysis and Modeling of Inertial Sensors Using Allan Variance,” IEEE Transactions on Instrumentation and Measurement, Vol. 57, No. 1, 2008, pp. 140–149. https://doi.org/10.1109/TIM.2007.908635 CrossrefGoogle Scholar[19] Lam Q., Stamatakos N., Woodruff C. and Ashton S., “Gyro Modeling and Estimation of Its Random Noise Sources,” AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA Paper 2003-5562, 2003. https://doi.org/10.2514/6.2003-5562 Google Scholar[20] Shuster M. D., “A Survey of Attitude Representations,” Navigation, Vol. 8, No. 9, 1993, pp. 439–517. Google Scholar[21] Kuipers J. B., Quaternions and Rotation Sequences, Princeton Univ. Press, Princeton, NJ, 1999, Chap. 5. https://doi.org/10.1515/9780691211701 CrossrefGoogle Scholar[22] Duan G.-R. and Yu H.-H., LMIs in Control Systems, CRC Press, Boca Raton, FL, 2013, pp. 296–297. https://doi.org/10.1201/b15060 Google Scholar[23] Apkarian P., Tuan P. H. D. and Bernussou J., “Continuous-Time Analysis, Eigenstructure Assignment, and H/sub 2/Synthesis with Enhanced Linear Matrix Inequalities (LMI) Characterizations,” IEEE Transactions on Automatic Control, Vol. 46, No. 12, 2001, pp. 1941–1946. https://doi.org/10.1109/9.975496 CrossrefGoogle Scholar[24] Grant M. and Boyd S., “CVX: Matlab Software for Disciplined Convex Programming, Version 2.1,” March 2014, http://cvxr.com/cvx. Google Scholar[25] Gu D.-W., Petkov P. and Konstantinov M. M., Robust Control Design with MATLAB®, Springer Science & Business Media, 2005, Chaps. 8–13. https://doi.org/10.1007/b135806 Google Scholar[26] “MPU-9250 Product Specification Revision 1.1,” InvenSense, 2016, http://www.invensense.com/wp-content/uploads/2015/02/PS-MPU-9250A-01-v1.1.pdf [retrieved 13 Nov. 2019]. Google Scholar[27] “Sensor Fusion and Tracking Toolbox,” MATLAB, 2018, https://www.mathworks.com/products/sensor-fusion-and-tracking.html [retrieved 18 Sept. 2019]. Google Scholar Previous article Next article FiguresReferencesRelatedDetailsCited byAdaptive Nonlinear Incremental Flight Control for Systems With Unknown Control EffectivenessIEEE Transactions on Aerospace and Electronic Systems, Vol. 59, No. 1Active Fault-Tolerant Incremental Sliding-Mode Flight Control Against Control ReversalJing Chang, Roeland De Breuker and Xuerui Wang 25 October 2022 | Journal of Guidance, Control, and Dynamics, Vol. 45, No. 12EKF-AF PID-Based Attitude Control Algorithm for UAVsMobile Information Systems, Vol. 2022Simultaneous Localization and Mapping (SLAM) and Data Fusion in Unmanned Aerial Vehicles: Recent Advances and Challenges28 March 2022 | Drones, Vol. 6, No. 4 What's Popular Volume 44, Number 2February 2021 CrossmarkInformationCopyright © 2020 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 eISSN 1533-3884 to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAircraft OperationsAircraft Operations and TechnologyAircraftsApplied MathematicsEarth SciencesElectromagnetismElementary AlgebraGeneral PhysicsGeometry FunctionsGeophysicsMagnetismMagnetometersMathematical OptimizationTakeoff and LandingUnmanned Aerial VehicleVertical Takeoff and Landing KeywordsQuaternionsExtended Kalman FilterMagnetometersAccelerometerGyroscopesMATLABNonlinear SystemsUAVMicroprocessorsSensor FusionAcknowledgmentsThis project has been supported by National Science Foundation (NSF) grants #1762825 and Improving Undergraduate STEM Education (IUSE) and Professional Formation of Engineers (PFE) IUSE/PFE: RED: Revolutionizing Diversity of Engineering [REDO-E] Award Number 1730693.PDF Received4 February 2020Accepted5 September 2020Published online28 October 2020
更多
查看译文
AI 理解论文
溯源树
样例
生成溯源树,研究论文发展脉络
Chat Paper
正在生成论文摘要