Numerical Optimization of Flight Trajectory for Rockets via Artificial Neural Networks
This research arise to optimize the flight trajectory for rockets, for this were applied hybrid techniques, based on the Finite Difference Method (FDM) to obtain the solution of the non-linear differential equations provided by the analytic modeling. So aiming at the optimizations were applied the A...
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Veröffentlicht in: | Revista IEEE América Latina 2017-01, Vol.15 (8), p.1556-1565 |
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Format: | Artikel |
Sprache: | eng |
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