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.

References

Downloads

Published

2020-10-23

Issue

No. 4 (2020): Modeling, control and information technologies: Proceedings of IV International scientific and practical conference

Section

Problems of automated control, optimization and parameters identification

How to Cite

Calculation of Flight Data Fusion Coefficients Using Newton–Raphson Iterations. (2020). MCIT: Proceedings of International Scientific and Practical Conference, 4, 100-103. https://doi.org/10.31713/MCIT.2020.20

Most read articles by the same author(s)