Simulation flight trajectory of the missle type accular corrected by the one-time lateral pulse engine matrix
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https://doi.org/10.54939/1859-1043.j.mst.77.2022.161-169Keywords:
Flight dynamics; Pulse motor matrix; Surface-to-surface missile.Abstract
On the basis of the mathematical model of the missile’s motion, the authors proposed the working algorithm of the pulse engine matrix controller to correct the flight trajectory of the missile following the nominal flight trajectory. The simulation results show that the algorithm for controlling the pulse motor matrix by each channel to track the nominal trajectory, ensuring the circular error probable is less than 10m, even when there are impacts of input noise such as initial launch angle deviation, measurement error of wind.
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