Neural Network Assisted Inverse Dynamic Guidance for Terminally Constrained Entry Flight

Table 3

Monte Carlo simulation results.

Parameter	Miss distance	Δ𝛾𝑓	Δ𝜓𝑓	Δ𝑣𝑓
Maximum	159 m	0.002°	0.02°	19.8 m/sec
Mean	0.22 m	0.0001°	0.002°	5.01 m/sec
Std. deviation	4.54 m	0.001°	0.003°	7.23 m/sec