Calculation of Flight Data Fusion Coefficients Using Newton–Raphson Iterations
Keyword(s):
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.
2009 ◽
Vol 49
(3)
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pp. 474-481
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2010 ◽
Vol 2010
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pp. 1-6
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1997 ◽
Vol 13
(1)
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pp. 33-44
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2019 ◽
Vol 1158
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pp. 032011