Abstract
Hypothesis, internal, and output paths of the airborne, seaborne, and ground-based objects in a complex informational environment (low probability of detection, uncertainty and incompleteness of coordinates, maneuvering and group objects) onboard an aircraft are discussed. All measurements of internal and external sources operating in survey, passive detection, and tracking modes are used for calculation. For external sources the composition of transmitted data is determined. In the partial measurement of the coordinates, a complex aircraft control system is formed, which increases the accuracy of the paths of such objects and puts the aircraft in the conditions of a rocket launch with the maximum range.
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