Reply by the Authors to P. J. Sherman

No AccessReplysReply by the Authors to P. J. ShermanHonglei Ji, Renliang Chen and Pan LiHonglei JiChongqing University, 400044 Chongqing, People’s Republic of China*Lecturer, College of Aerospace Engineering; (Corresponding Author).Search for more papers by this author, Renliang ChenNanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China†Professor, National Laboratory of Science and Technology on Rotorcraft Aeromechanics, College of Aerospace Engineering, Jiangsu; (Corresponding Author).Search for more papers by this author and Pan LiNanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China‡Associate Professor, National Laboratory of Science and Technology on Rotorcraft Aeromechanics, College of Aerospace Engineering, Jiangsu; .Search for more papers by this authorPublished Online:16 Feb 2021https://doi.org/10.2514/1.C036264SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Sherman P. J., “Comment on ‘Analysis of Helicopter Handling Quality in Turbulence with Recursive von Kármán Model’,” Journal of Aircraft, Vol. XX, No. XX, 2020, pp. XXX–XXX. Google Scholar[2] Ji H., Chen R. and Li P., “Analysis of Helicopter Handling Quality in Turbulence with Recursive von Kármán Model,” Journal of Aircraft, Vol. 54, No. 5, 2017, pp. 1631–1639. https://doi.org/10.2514/1.C034189 LinkGoogle Scholar[3] McFarland R. E. and Duisenberg K., “Simulation of Rotor Blade Element Turbulence,” NASA TM-108862, 1995. Google Scholar[4] Ji H., Chen R. and Li P., “Distributed Atmospheric Turbulence Model for Helicopter Flight Simulation and Handling Quality Analysis,” Journal of Aircraft, Vol. 54, No. 1, 2017, pp. 190–198. https://doi.org/10.2514/1.C033667 LinkGoogle Scholar[5] Ji H., Chen R. and Li P., “Distributed Turbulence Model with Rigorous Spatial Cross-Correlation for Simulation of Helicopter Flight in Atmospheric Turbulence,” Journal of the American Helicopter Society, Vol. 64, No. 4, 2019, Paper 042011. https://doi.org/10.4050/JAHS.64.042011 CrossrefGoogle Scholar[6] Ji H., Chen R. and Li P., “Real-Time Simulation Model for Helicopter Flight Task Analysis in Turbulent Atmospheric Environment,” Aerospace Science and Technology, Vol. 92, Sept. 2019, pp. 289–299. https://doi.org/10.1016/j.ast.2019.05.066 CrossrefGoogle Scholar[7] Gaonkar G. H., “A Perspective on Modelling Rotorcraft in Turbulence,” Probabilistic Engineering Mechanics, Vol. 3, No. 1, 1988, pp. 36–42. https://doi.org/10.1016/0266-8920(88)90006-9 CrossrefGoogle Scholar[8] Brown R. G. and Hwang P. Y. C., Introduction to Random Signals and Applied Kalman Filtering, 4th ed., Wiley, Hoboken, NJ, 2012, Chaps. 1, 2. Google Scholar[9] Hess R. A. and Siwakosit W., “Assessment of Flight Simulator Fidelity in Multiaxis Tasks Including Visual Cue Quality,” Journal of Aircraft, Vol. 38, No. 4, 2001, pp. 607–614. https://doi.org/10.2514/2.2836 LinkGoogle Scholar[10] Lusardi J. A., Tischler M. B., Blanken C. L. and Labows S. J., “Empirically Derived Helicopter Response Model and Control System Requirements for Flight in Turbulence,” Journal of the American Helicopter Society, Vol. 49, No. 3, 2004, pp. 340–349. https://doi.org/10.4050/JAHS.49.340 CrossrefGoogle Scholar Previous article Next article FiguresReferencesRelatedDetails What's Popular Volume 58, Number 2March 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 1533-3868 to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAerodynamicsAeronautical EngineeringAeronauticsAircrewAviationCivil AviationCommercial AviationComputing, Information, and CommunicationSignal ProcessingTurbulenceTurbulence Models KeywordsPower Spectral DensityWhite NoiseTurbulence ModelsPilotAcknowledgmentsThe authors acknowledge the financial support of the National Natural Science Foundation of China (grant 11902052), the Chongqing Science and Technology Bureau (grant cstc2019jscx-msxmX0043), and the National Laboratory of Science and Technology on Rotorcraft Aeromechanics (grant JZX7Y201911SY004001).PDF Received30 October 2020Accepted3 December 2020Published online16 February 2021