FRINK Linked Data Fragments server

Matches in SemOpenAlex for { <https://semopenalex.org/work/W2810596543> ?p ?o ?g. }

• W2810596543 endingPage "2257" @default.
• W2810596543 startingPage "2247" @default.
• W2810596543 abstract "No 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*Aerospace Engineer. Senior Member AIAA.Search for more papers by this author, Mark B. TischlerU.S. Army Aviation Development Directorate, Moffett Field, California 94035†Flight Control Technology Group Leader, Senior Scientist. Associate Fellow AIAA.Search for more papers by this author, Marit E. KnappU.S. Army Aviation Development Directorate, Moffett Field, California 94035‡Research Associate, San Jose State University Research Foundation. Member AIAA.Search for more papers by this author and Mark J. S. LopezU.S. Army Aviation Development Directorate, Moffett Field, California 94035§Aerospace Engineer. Member AIAA.Search for more papers by this authorPublished 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" @default.
• W2810596543 created "2018-07-10" @default.
• W2810596543 creator A5002123814 @default.
• W2810596543 creator A5016790708 @default.
• W2810596543 creator A5059269635 @default.
• W2810596543 creator A5078697349 @default.
• W2810596543 date "2018-10-01" @default.
• W2810596543 modified "2023-09-29" @default.
• W2810596543 title "Identification of Multi-Input Systems in the Presence of Highly Correlated Inputs" @default.
• W2810596543 cites W1998440482 @default.
• W2810596543 cites W2000564230 @default.
• W2810596543 cites W2123263215 @default.
• W2810596543 cites W2135768597 @default.
• W2810596543 cites W2152633755 @default.
• W2810596543 cites W2320709628 @default.
• W2810596543 cites W2498803165 @default.
• W2810596543 cites W2561780642 @default.
• W2810596543 cites W2567971972 @default.
• W2810596543 cites W2568356853 @default.
• W2810596543 cites W2570195219 @default.
• W2810596543 cites W2782122019 @default.
• W2810596543 doi "https://doi.org/10.2514/1.g003530" @default.
• W2810596543 hasPublicationYear "2018" @default.
• W2810596543 type Work @default.
• W2810596543 sameAs 2810596543 @default.
• W2810596543 citedByCount "15" @default.
• W2810596543 countsByYear W28105965432019 @default.
• W2810596543 countsByYear W28105965432020 @default.
• W2810596543 countsByYear W28105965432022 @default.
• W2810596543 countsByYear W28105965432023 @default.
• W2810596543 crossrefType "journal-article" @default.
• W2810596543 hasAuthorship W2810596543A5002123814 @default.
• W2810596543 hasAuthorship W2810596543A5016790708 @default.
• W2810596543 hasAuthorship W2810596543A5059269635 @default.
• W2810596543 hasAuthorship W2810596543A5078697349 @default.
• W2810596543 hasConcept C116834253 @default.
• W2810596543 hasConcept C119247159 @default.
• W2810596543 hasConcept C124101348 @default.
• W2810596543 hasConcept C2780009758 @default.
• W2810596543 hasConcept C41008148 @default.
• W2810596543 hasConcept C59822182 @default.
• W2810596543 hasConcept C86803240 @default.
• W2810596543 hasConceptScore W2810596543C116834253 @default.
• W2810596543 hasConceptScore W2810596543C119247159 @default.
• W2810596543 hasConceptScore W2810596543C124101348 @default.
• W2810596543 hasConceptScore W2810596543C2780009758 @default.
• W2810596543 hasConceptScore W2810596543C41008148 @default.
• W2810596543 hasConceptScore W2810596543C59822182 @default.
• W2810596543 hasConceptScore W2810596543C86803240 @default.
• W2810596543 hasIssue "10" @default.
• W2810596543 hasLocation W28105965431 @default.
• W2810596543 hasOpenAccess W2810596543 @default.
• W2810596543 hasPrimaryLocation W28105965431 @default.
• W2810596543 hasRelatedWork W15554183 @default.
• W2810596543 hasRelatedWork W176335707 @default.
• W2810596543 hasRelatedWork W2076328977 @default.
• W2810596543 hasRelatedWork W2312738077 @default.
• W2810596543 hasRelatedWork W2382161936 @default.
• W2810596543 hasRelatedWork W2803979147 @default.
• W2810596543 hasRelatedWork W3108133766 @default.
• W2810596543 hasRelatedWork W4248817909 @default.
• W2810596543 hasRelatedWork W4252600690 @default.
• W2810596543 hasRelatedWork W4367048510 @default.
• W2810596543 hasVolume "41" @default.
• W2810596543 isParatext "false" @default.
• W2810596543 isRetracted "false" @default.
• W2810596543 magId "2810596543" @default.
• W2810596543 workType "article" @default.