Abstract

Estimating parameters from flight data having both the measurement and process noise poses difficulties with most of the available parameter estimation methods. For such flight data, a recently proposed neural network based parameter estimation method '(called the Delta method) is used for extraction of longitudinal parameters. Results are presented for simulated flight data in turbulent atmosphere, and it is shown that the Delta method estimates are good even from flight data in severe turbulence and also having measurement noise in them. For nonlinear terms present in the aerodynamic model, a frequency-domain application of the Delta method is also illustrated. A comparison of estimates via the Delta method with those via the output error method and time varying filter error approach is presented. Nomenclature

Full Text
Paper version not known

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call

Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.