FIELD: aviation.
SUBSTANCE: on the basis of autonomous reconfiguration of architecture and structure of the navigation complex (NC), it is possible to continue the flight and complete the mission in the presence of several failed elements in the NC structure. The NC is operated without ground control equipment. NC contains an integrated sensor unit made three or more times redundant, magnetometric sensor, an air signal system, a satellite navigation system, a radio navigation system, a laser rangefinder, an optoelectronic and astronavigation system. Three or more times redundant computing devices, three or more times redundant units of redundant navigation, three or more times redundant software algorithmic modules for quorumizing and reconfiguring each channel of the input and output sections of control signals, sensors and reserve computers, three or more times redundant database storage units for software and algorithmic support (SAS) of initial training modes, three or more times redundant database storage units of sensor models and on-board navigation systems, and three or more times redundant storage units for SAS of complex information processing.
EFFECT: expansion of the functionality of navigation complex, increase of survivability, reliability and fail-safety of integrated navigation.
2 cl, 1 dwg
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Authors
Dates
2018-01-12—Published
2016-07-20—Filed