Identification of Multi-Input Systems in the Presence of Highly Correlated Inputs
2018; American Institute of Aeronautics and Astronautics; Volume: 41; Issue: 10 Linguagem: Inglês
10.2514/1.g003530
ISSN1533-3884
AutoresTom Berger, Mark B. Tischler, Marit E. Knapp, Mark J. S. Lopez,
Tópico(s)Probabilistic and Robust Engineering Design
ResumoNo AccessEngineering NoteIdentification of Multi-Input Systems in the Presence of Highly Correlated InputsTom Berger, Mark B. Tischler, Marit E. Knapp and Mark J. S. LopezTom BergerU.S. Army Aviation Development Directorate, Moffett Field, California 94035, Mark B. TischlerU.S. Army Aviation Development Directorate, Moffett Field, California 94035, Marit E. KnappU.S. Army Aviation Development Directorate, Moffett Field, California 94035 and Mark J. S. LopezU.S. Army Aviation Development Directorate, Moffett Field, California 94035Published Online:29 Jun 2018https://doi.org/10.2514/1.G003530SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Tischler M. B. and Remple R. K., Aircraft and Rotorcraft System Identification: Engineering Methods and Flight Test Examples, 2nd ed., AIAA, Reston, VA, 2012, Chap. 9. doi:https://doi.org/10.2514/4.868207 LinkGoogle Scholar[2] Morelli E. and Klein V., Aircraft System Identification—Theory and Practice, 2nd ed., Sunflyte Enterprises, Williamsburg, VA, 2016, Chap. 7. Google Scholar[3] Zivan L. and Tischler M. B., "Development of a Full Flight Envelope Helicopter Simulation Using System Identification," Journal of the American Helicopter Society, Vol. 55, No. 2, 2010, Paper 22003. doi:https://doi.org/10.4050/JAHS.55.022003 JHESAK 0002-8711 CrossrefGoogle Scholar[4] Grauer J. and Morelli E., "Method for Real-Time Frequency Response and Uncertainty Estimation," Journal of Guidance, Navigation, and Control, Vol. 37, No. 1, 2014, pp. 336–343. doi:https://doi.org/10.2514/1.60795 LinkGoogle Scholar[5] Jung S., Shim D. H. and Kim E.-T., "Helicopter Dynamic Model Identification by Conditional Attitude Hold Logic," AIAA Paper 2017-1251, 2017. doi:https://doi.org/10.2514/6.2017-1251 LinkGoogle Scholar[6] Forssell U. and Ljung L., "Closed-Loop Identification Revisited," Automatica, Vol. 35, No. 7, 1999, pp. 1215–1241. doi:https://doi.org/10.1016/S0005-1098(99)00022-9 ATCAA9 0005-1098 CrossrefGoogle Scholar[7] Akaike H., "Some Problems in the Application of the Cross-Spectral Method," Spectral Analysis of Time Series, edited by Harris B., Wiley, New York, 1967, pp. 81–107. Google Scholar[8] Gennaretti M., Gori R., Serafini J., Cardito F. and Bernardini G., "Identification of Rotor Wake Inflow Finite-State Models for Flight Dynamics Simulations," CEAS Aeronautical Journal, Vol. 8, No. 1, 2017, pp. 209–230. doi:https://doi.org/10.1007/s13272-016-0235-y CrossrefGoogle Scholar[9] Hersey S., Celi R., Juhasz O., Tischler M. B., Rand O. and Khromov V., "State-Space Inflow Model Identification and Flight Dynamics Coupling for an Advanced Coaxial Rotorcraft Configuration," 73rd American Helicopter Society Annual Forum [CD-ROM], AHS International, Alexandria, VA, 2017. Google Scholar[10] Knapp M. E., Berger T., Tischler M. B. and Cotting M. C., "Development of a Full Envelope Flight Identified F-16 Simulation Model," AIAA Paper 2018-0525, 2018. doi:https://doi.org/10.2514/6.2018-0525 LinkGoogle Scholar[11] Berger T., Tischler M. B., Hagerott S. G., Cotting M. C., Gresham J. L., George J. E., Krogh K. J., D'Argenio A. and Howland J. D., "Development and Validation of a Flight Identified Business Jet Simulation Model Using a Stitching Architecture," AIAA Paper 2017-1550, 2017. doi:https://doi.org/10.2514/6.2017-1550 LinkGoogle Scholar[12] Tischler M. B., Berger T., Ivler C. M., Mansur M. H., Cheung K. K. and Soong J. Y., Practical Methods for Aircraft and Rotorcraft Flight Control Design: An Optimization-Based Approach, AIAA, Reston, VA, 2017, pp. 249–257. doi:https://doi.org/10.2514/4.104435 Google Scholar[13] Morelli E. A. and Smith M. S., "Real-Time Dynamic Modeling: Data Information Requirements and Flight-Test Results," Journal of Aircraft, Vol. 46, No. 1, 2009, pp. 1894–1905. doi:https://doi.org/10.2514/1.40764 LinkGoogle Scholar[14] Tischler M. B., Ivler C. M. and Berger T., "Comment on 'Method for Real-Time Frequency Response and Uncertainty Estimation'," Journal of Guidance, Control, and Dynamics, Vol. 38, No. 3, 2015, pp. 547–549. doi:https://doi.org/10.2514/1.G000780 JGCODS 0731-5090 LinkGoogle Scholar[15] Berger T., Tischler M. B., Hagerott S. G., Gangsaas D. and Saeed N., "Lateral/Directional Control Law Design and Handling Qualities Optimization for a Business Jet Flight Control System," AIAA Paper 2013-4506, 2013. doi:https://doi.org/10.2514/6.2013-4506 LinkGoogle Scholar[16] Berger T., Tischler M. B., Hagerott S. G., Cotting M. C., Gresham J. L., George J. E., Krogh K. J., D'Argenio A. and Howland J. D., "Handling Qualities Flight Test Assessment of a Business Jet NzU P−β Fly-By-Wire Control System," AIAA Paper 2017-1398, 2017. doi:https://doi.org/10.2514/6.2017-1398 LinkGoogle Scholar Previous article Next article FiguresReferencesRelatedDetailsCited byAerodynamic characterisation of delta wing unmanned aerial vehicle using non-gradient-based estimator23 February 2023 | The Aeronautical Journal, Vol. 93Efficient Frequency Response Identification for Small Fixed-Wing UAS Using Closed-Loop Flight DataJustin Matt and Haiyang Chao19 January 2023Flight Control Technology Advancements and Challenges for Future Rotorcraft 40th Alexander A. Nikolsky Honorary LectureJournal of the American Helicopter Society, Vol. 67, No. 4System identification of cropped delta UAVs from flight test methods using particle Swarm-Optimisation-based estimation4 May 2022 | The Aeronautical Journal, Vol. 110Frequency Response Estimation for Multiple Aircraft Control Loops Using Orthogonal Phase-Optimized Multisine Inputs22 March 2022 | Processes, Vol. 10, No. 4Aircraft System Identification from Multisine Inputs and Frequency ResponsesJared A. Grauer and Matthew J. Boucher2 September 2020 | Journal of Guidance, Control, and Dynamics, Vol. 43, No. 12The LOES-based control scheme of aerospace vehicle under flying quality constraintsActa Astronautica, Vol. 177Identification of a Full-Envelope Learjet-25 Simulation Model Using a Stitching ArchitectureTom Berger, Mark B. Tischler, Steven G. Hagerott, M. Christopher Cotting and William R. Gray25 August 2020 | Journal of Guidance, Control, and Dynamics, Vol. 43, No. 11Multi-Axis Inputs for Identification of a Reconfigurable Fixed-Wing UAV5 August 2020 | Aerospace, Vol. 7, No. 8Real-Time Estimation of Bare-Airframe Frequency Responses from Closed-Loop Data and Multisine InputsJared A. Grauer and Matthew J. Boucher24 September 2019 | Journal of Guidance, Control, and Dynamics, Vol. 43, No. 2Frequency Responses Identification from Multi-Axis Maneuver with Simultaneous Multisine InputsPiotr Lichota, Joanna Szulczyk, Mark B. Tischler and Tom Berger24 June 2019 | Journal of Guidance, Control, and Dynamics, Vol. 42, No. 11Identification of Bare-Airframe Dynamics from Closed-Loop Data Using Multisine Inputs and Frequency ResponsesJared A. Grauer and Matthew Boucher6 January 2019 What's Popular Volume 41, Number 10October 2018 CrossmarkInformationThis material is declared a work of the U.S. Government and is not subject to copyright protection in the United States. 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. TopicsAircraft Components and StructureAircraft DesignAircraft Operations and TechnologyAircraft Stability and ControlAircraftsControl SystemsControl TheoryFeedback ControlFlight Control SurfacesGuidance, Navigation, and Control SystemsHelicoptersJet AircraftRotorcrafts KeywordsSingle Input Single OutputYaw DamperClosed Loop SystemAirframesFlight TestingSideslipCopilotDutch RollFlight DataFrequency DomainPDF Received21 December 2017Accepted7 April 2018Published online29 June 2018
Referência(s)