Inertia technique is a high and new technology, which is also a basic supporting technology used in astronavigation, aviation, navigation and modern weapon system. Main performance parameters of inertia system are described in positioning accuracy, course accuracy, attitude accuracy and rate accuracy, and these performance parameters are tested and calibrated with different inertial navigation test equipments. This paper, according to the full automatic three-dimensional multi-functiori inertial navigation test system developed for calibration of some type tactical missile inertial assemble, introduces the design method of all parts of inertial navigation test system, and analyses several key techniques which are related to the system.
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