FIELD: navigation, control and guidance of multi-functional flying vehicles.
SUBSTANCE: proposed complex includes several information control complexes combined in single information control system by means of information exchange channels. Each complex includes radar navigation unit, observation sighting units, natural and artificial field image identification systems, inertial sensors and systems, air (aerometric) sensors and systems, indication control units, relative coordinate determination unit, communication units and computer system for input and output of information and automatic information exchange control, calculation of information parameters of state and motion of flying vehicle, complex processing of information and obtaining information on surrounding space (geophysical fields, state and motion of atmosphere, reference points) and associated objects, synthesis of parameters of any flying vehicle and surrounding space. Computer system includes information input and output units, parameter forming units (coordinates, speed, acceleration, angular orientation of inertial space, Earth, atmosphere, reference points and associated objects), information processing units, synthesis of parameters of state and surrounding space, calculation of parameters of relative motion of flying vehicles. All information pertaining to state of flying vehicle group is transmitted to all groups by means of information exchange channels.
EFFECT: simplified integration of systems of individual flying vehicles, enhanced stability.
1 dwg
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Authors
Dates
2004-07-10—Published
2003-10-21—Filed