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 value	Rosenbrock method		RTPEC-34 method (13c)
		0	1.0000	1.0000	1.0000	1.0000	1.0000
0.1	1.0101	1.0075	1.0049	1.0050	1.0100
0.2	1.0408	1.0355	1.0303	1.0405	1.0300
0.3	1.0942	1.0859	1.0777	1.0991	1.0822
0.4	1.1735	1.1617	1.1501	1.1843	1.1714
0.5	1.2840	1.2679	1.2522	1.3019	1.2934
0.6	1.4333	1.4118	1.3910	1.4601	1.4567
0.7	1.6323	1.6038	1.5765	1.6705	1.6737
0.8	1.8965	1.8588	1.8228	1.9498	1.9616
0.9	2.2479	2.1978	2.1501	2.3217	2.3451
1.0	2.7183	2.6511	2.5875	2.8203	2.8599