The Scientific World Journal / 2014 / Article / Tab 2

Research Article

Neural Network Assisted Inverse Dynamic Guidance for Terminally Constrained Entry Flight

Table 2

The perturbations in Monte Carlo run.

ParameterValue

Range±1.5 km
Altitude±1.5 km
Cross range±1.5 km
Aerodynamic modelling±10%
Velocity±75 m/sec
Flight path angle±0.06°
Azimuth angle±0.06°
Atmospheric modelling±10%