In the radar tracking using Kalman filter example (aero_radmod_dsp), what are the dynamic equations used to model XY acceleration for the aircraft?
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I am trying to create a similar project but the documentation of the example doesn't provide any information about the dynamics of the aircraft and the constants that are being used.
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Vladimir Cheremushkin
2018 年 7 月 15 日
編集済み: Vladimir Cheremushkin
2018 年 7 月 15 日
For CB. Hi! If you use this example (below, reference), then there is a system from two equations. These two equations are in a matrix form.
https://www.mathworks.com/examples/matlab-dsp-system/mw/dsp_product-aircraftPositionEstimateExampleApp-estimating-position-of-an-aircraft-using-kalman-filter
More general form of this system of the equations (form of State Space) has been written in work (article) R. Kalman (1960). Can you show the code for the MATLAB environment here? There is Filtеr of Kalman?
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