Abstract: The analysis of errors and computation on air to air missile launch and control parameters are an important link to ensure an effective attack. The lead pursuit attack mode is described and a model to compute missile launch and control parametersis given. The computer simulation constructure of missile delivery errors analysis is established and the sensitivities of the missile launch and control parameters to error sources are studied based on the small perturbation method.

Key words: air to air missile, missile launching, error analysis