Neural Network Assisted Inverse Dynamic Guidance for Terminally Constrained Entry Flight

Table 2

The perturbations in Monte Carlo run.

Parameter	Value
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%