The Scientific World Journal / 2014 / Article / Tab 3

Research Article

Neural Network Assisted Inverse Dynamic Guidance for Terminally Constrained Entry Flight

Table 3

Monte Carlo simulation results.

ParameterMiss distance

Maximum159 m0.002°0.02°19.8 m/sec
Mean0.22 m0.0001°0.002°5.01 m/sec
Std. deviation4.54 m0.001°0.003°7.23 m/sec