Calculation of Flight Data Fusion Coefficients Using Newton–Raphson Iterations

Authors

DOI:

https://doi.org/10.31713/MCIT.2020.20

Keywords:

mathematical model, data fusion, aircraft, black box, differential equations, iteration method

Abstract

The problem of plotting the flight path of an aircraft based on flight data containing numerous measurement errors is investigated. A theoretical (continuous) model of the flight data fusion problem is proposed in the form of a boundary value problem for a system of differential equations with unknown coefficients. The application of the Newton–Raphson iteration method for calculating the sought-for coefficients is described.

Downloads

Published

2020-10-23

How to Cite

Sabziev, E. N. (2020). Calculation of Flight Data Fusion Coefficients Using Newton–Raphson Iterations. Modeling, Control and Information Technologies, (4), 100–103. https://doi.org/10.31713/MCIT.2020.20

Issue

No. 4 (2020): Modeling, control and information technologies

Section

Problems of automated control, optimization and parameters identification

License

All materials are distributed under the terms of the Creative Commons Attribution 4.0 International License, which allows others to distribute the work with attribution to the authorship of this work and the first publication in this journal.