Mathematical Problems in Engineering / 2015 / Article / Tab 1

Research Article

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

Table 1

Parameter values obtained using different optimization methods.

ParameterFDMQPGA with a punishment strategy

0.39590.54500.5181
1.55340.91220.9963
−0.68110.12330.0125
0.1403−0.0681−0.0337
−0.01260.03260.0249
0.52390.79470.7425
−0.1775−0.3510−0.3147
0.04950.10120.0903

We are committed to sharing findings related to COVID-19 as quickly as possible. We will be providing unlimited waivers of publication charges for accepted research articles as well as case reports and case series related to COVID-19. Review articles are excluded from this waiver policy. Sign up here as a reviewer to help fast-track new submissions.