Mathematical Problems in Engineering / 2015 / Article / Tab 3

Research Article

An Accurate Method for Real-Time Aircraft Dynamics Simulation Based on Predictor-Corrector Scheme

Table 3

Comparison of numerical solutions obtained with different step sizes.

Theoretical valueRosenbrock methodRTPEC-34 method (13c)

01.00001.00001.00001.00001.0000
0.11.01011.00751.00491.00501.0100
0.21.04081.03551.03031.04051.0300
0.31.09421.08591.07771.09911.0822
0.41.17351.16171.15011.18431.1714
0.51.28401.26791.25221.30191.2934
0.61.43331.41181.39101.46011.4567
0.71.63231.60381.57651.67051.6737
0.81.89651.85881.82281.94981.9616
0.92.24792.19782.15012.32172.3451
1.02.71832.65112.58752.82032.8599

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