complexity in the perspective of the model and the necessary initial states and parameters:

o Six-Degrees-of-Freedom rigid body (6DoF)

o Modified-Linear Theory (MLT)

o Modified Point Mass (MPM)

o Full Point Mass (FPM)

o Simple Point Mass (SPM)

o Hybrid Point Mass (HPM)

o Vacuum Point Mass (VPM)

Guidance methods for ballistic missiles are used to compensate for the difficulty in pre-launch prediction, which originates from uncertainties in maneuvering. In these, machine learning

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