Inverse Problem of Dynamics: The Algorithm for Identifying the Parameters of an Aircraft

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Abstract

The development of efficient parameter identification methods for the model of a dynamic system based on real-time measurements of some components of its state vector should be taken as one of the most important problems of applied statistics and computational mathematics. Calculating the motion of the system given the initial conditions and its mathematical model is conventionally called the direct problem of dynamics.

Keywords

Kalman Filter Motion Equation Wind Tunnel Experiment Aerodynamic Coefficient Aerodynamic Parameter 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.
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Copyright information

© Springer International Publishing Switzerland 2016

Authors and Affiliations

  1. 1.State Scientific Research Institute of Automated SystemsMoscowRussia

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