Tracking Filter Integration in the Adaptive Augmenting Controller of a Launch Vehicle
2021; American Institute of Aeronautics and Astronautics; Volume: 44; Issue: 12 Linguagem: Inglês
10.2514/1.g006007
ISSN1533-3884
AutoresDomenico Trotta, Alessandro Zavoli, G. De Matteis, Agostino Neri,
Tópico(s)Advanced Control Systems Optimization
ResumoNo AccessEngineering NotesTracking Filter Integration in the Adaptive Augmenting Controller of a Launch VehicleDomenico Trotta, Alessandro Zavoli, Guido De Matteis and Agostino NeriDomenico TrottaSapienza University of Rome, 00184 Rome, Italy*Ph.D. Student, Department of Mechanical and Aerospace Engineering, Via Eudossiana 18; .Search for more papers by this author, Alessandro ZavoliSapienza University of Rome, 00184 Rome, Italy†Research Fellow, Department of Mechanical and Aerospace Engineering, Via Eudossiana 18; .Search for more papers by this author, Guido De MatteisSapienza University of Rome, 00184 Rome, Italy‡Professor, Department of Mechanical and Aerospace Engineering, Via Eudossiana 18; .Search for more papers by this author and Agostino NeriESA/ESRIN (European Space Research Institute), I-00044 Frascati, Rome, Italy§Head of VEGA Programmes Coordination Office (STS-PVC), Vega Integrated Project Team, AIAA SRTC Vice-Chair & STTC Distinguished Technical Expert, ESA/ESRIN Largo Galileo Galilei, 1; . Associate Fellow AIAA.Search for more papers by this authorPublished Online:13 Aug 2021https://doi.org/10.2514/1.G006007SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Orr J., Wall J., VanZwieten T. and Hall C., “Space Launch System Ascent Flight Control Design (AAS 14-038),” Advances in the Astronautical Sciences, Vol. 151, Jan. 2014, pp. 141–154. Google Scholar[2] Haykin S., Adaptive Filter Theory, 5th ed., Pearson Education Ltd., Edinburgh Gate Harlow, England, U.K., 2014, Chap. 10. Google Scholar[3] Orr J. and Van Zwieten T., “Robust, Practical Adaptive Control for Launch Vehicles,” AIAA Guidance, Navigation, and Control Conference, AIAA Paper 2012-4549, 2012. https://doi.org/10.2514/6.2012-4549 LinkGoogle Scholar[4] Greensite A. L., “Analysis and Design of Space Vehicle Flight Control Systems. Volume VII-Attitude Control During Launch,” NASA CR-826, GD/C-DDE66-028, 1967. Google Scholar[5] Roux C. and Cruciani I., “Scheduling Schemes and Control Law Robustness in Atmospheric Flight of VEGA Launcher,” 7th International ESA Conference on Guidance, Navigation & Control Systems, European Space Agency, June 2008. Google Scholar[6] Wall J. H., Orr J. S. and VanZwieten T. S., “Space Launch System Implementation of Adaptive Augmenting Control,” 37th Annual American Astronautical Society (AAS) Guidance, Navigation, and Control Conference, American Astronautical Soc. Paper 14-051, Springfield, VA, 2014. Google Scholar[7] Trotta D., Zavoli A., De Matteis G. and Neri A., “Opportunities and Limitations of Adaptive Augmented Control for Launch Vehicle Attitude Control in Atmospheric Flight,” Astrodynamics Specialist Conference, American Astronautical Soc. Paper 19-765, Springfield, VA, 2019. Google Scholar[8] Trotta D., Zavoli A., De Matteis G. and Neri A., “Optimal Tuning of Adaptive Augmenting Controller for Launch Vehicles in Atmospheric Flight,” Journal of Guidance, Control, and Dynamics, Vol. 43, No. 11, 2020, pp. 2133–2140. https://doi.org/10.2514/1.g005352 LinkGoogle Scholar[9] Garner D., “Control Theory Handbook,” NASA TM-X-53036, NASA Marshall Space Flight Center, 1964. Google Scholar[10] Jang J.-W., Hall R., Bedrossian N. and Hall C., “Ares-I Bending Filter Design Using a Constrained Optimization Approach,” AIAA Guidance, Navigation and Control Conference and Exhibit, AIAA Paper 2008-6289, 2008. https://doi.org/10.2514/6.2008-6289 LinkGoogle Scholar[11] Leea S.-I., Ahn J. and Roh W.-R., “Integrated Design Optimization of Structural Bending Filter and Gain Schedules for Rocket Attitude Control System,” arXiv:1802.01875, 2018. Google Scholar[12] Cunningham C. and Higgins W., “Study of Applications of a Tracking Filter to Stabilize Large Flexible Launch Vehicles,” NASA CR-77353, 1966. Google Scholar[13] Gaylor R., Schaperkoetter R. L. and Cunningham D. C., “An Adaptive Tracking Filter for Bending-Mode Stabilization,” Journal of Spacecraft and Rockets, Vol. 4, No. 5, 1967, pp. 573–577. https://doi.org/10.2514/3.28911 LinkGoogle Scholar[14] Greensite A. L., “Analysis and Design of Space Vehicle Flight Control Systems. Volume XIII-Adaptive Control,” NASA CR-832, 1967, pp. 54–66. Google Scholar[15] Kharisov E., Gregory I., Cao C. and Hovakimyan N., “L1 Adaptive Control for Flexible Space Launch Vehicle and Proposed Plan for Flight Validation,” AIAA Guidance, Navigation and Control Conference and Exhibit, AIAA Paper 2008-7128, 2008. https://doi.org/10.2514/6.2008-7128 LinkGoogle Scholar[16] Ra W., “Practical Adaptive Notch Filter for Missile Bending Mode Rejection,” Electronics Letters, Vol. 41, No. 5, 2005, pp. 228–229. https://doi.org/10.1049/el:20057263 Google Scholar[17] Jafari A. A., Khoshnood A. M. and Roshanian J., “Model Reference Adaptive Method for Estimating the Bending Vibration Frequency of a Flexible System,” International MultiConference of Engineers and Computer Scientists, IMECS 2008, Vol. 2, IAENG International Assoc. of Engineers, Hong Kong, March 2008. Google Scholar[18] Brito A. G., Franca S. M. and Leite Filho W. C., “Varying-Time Notch Filter for Bending Modes Active Suppression in Aerospace Systems,” 7th ESA International Conference on Guidance, Navigation and Control Systems, European Space Agency, June 2008. Google Scholar[19] Choi H.-D. and Bang H., “An Adaptive Control Approach to the Attitude Control of a Flexible Rocket,” Control Engineering Practice, Vol. 8, No. 9, 2000, pp. 1003–1010. https://doi.org/10.1016/S0967-0661(00)00032-0 CrossrefGoogle Scholar[20] Oh C.-S., Bang H. and Park C.-S., “Attitude Control of a Flexible Launch Vehicle Using an Adaptive Notch Filter: Ground Experiment,” Control Engineering Practice, Vol. 16, No. 1, 2008, pp. 30–42. https://doi.org/10.1016/j.conengprac.2007.03.006 CrossrefGoogle Scholar[21] Wie B. and Byun K.-W., “New Generalized Structural Filtering Concept for Active Vibration Control Synthesis,” Journal of Guidance, Control, and Dynamics, Vol. 12, No. 2, 1989, pp. 147–154. https://doi.org/10.2514/3.20384 LinkGoogle Scholar[22] Navarro Tapia D., Marcos A., Bennani S. and Roux C., “Joint Robust Structured Design of VEGA Launcher’s Rigid-Body Controller and Bending Filter,” Proceedings of the 69th International Astronautical Congress, International Astronautical Federation (IAF) Paper IAC-18,C1,5,3,x45007, Paris, France, Oct. 2018. Google Scholar[23] Johnson D., “Terrestrial Environment (Climatic) Criteria Guidelines for Use in Aerospace Vehicle Development. 2008 Revision,” NASA TM 2008-215633, 2008. Google Scholar[24] Simplcio P., Bennani S., Marcos A., Roux C. and Lefort X., “Structured Singular-Value Analysis of the VEGA Launcher in Atmospheric Flight,” Journal of Guidance, Control, and Dynamics, Vol. 39, No. 6, 2016, pp. 1342–1355. https://doi.org/10.2514/1.G000335 Google Scholar Previous article FiguresReferencesRelatedDetails What's Popular Volume 44, Number 12December 2021 CrossmarkInformationCopyright © 2021 by the authors. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. 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. TopicsAerodynamic PerformanceAerodynamicsComputational Fluid DynamicsFluid DynamicsMechanical and Structural VibrationsMonte Carlo MethodNumerical AnalysisRunge-Kutta MethodsStructural AnalysisStructural Design and DevelopmentStructural EngineeringStructural Kinematics and DynamicsStructures, Design and Test KeywordsSatellite Launch VehicleThrust Vector ControlOpen Loop Transfer FunctionAdaptive FilterInertial Navigation SystemFlight Control SystemStructural LoadRigid Body DynamicsAerodynamic CoefficientsSounding RocketsAcknowledgmentThis work was supported by ESA/ESRIN under Grant No. 4000120618/17/I/AL.PDF Received17 February 2021Accepted1 July 2021Published online13 August 2021
Referência(s)