Mathematical Problems in Engineering / 2015 / Article / Tab 2

Research Article

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

Table 2

Numerical errors due to different values of the parameters in (13a), (13b), and (13c).

Formula (13a)Formula (13b)Formula (13c)
(FDM)(QR)(GA with a punishment strategy)

0.0000
0.0200
0.0400
0.0600
0.0800
0.1000
0.1200
0.1400
0.1600
0.1800
0.2000

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