FIELD: control and navigational equipment.
SUBSTANCE: the invention refers to the sphere of control and navigation and may be used on flying vehicles of different types and functions: aircraft, helicopters, airfoil boats and airships and also on water and land transportation vehicles. Integrated flight-navigational complex has an inertial navigational system 1 and a satellite navigational system of automatic dependant observation 2, sensors of air parameters system 3, computing system 4, a system of input data and executive instructions 5, connected to the computing system, a multifunctional system of indication and signaling 6 , a concentrator 7, a computer 8, a bus of data exchange 9, adapters 10,interface modules 11, drives 12 and sensors 13 of a flight control system, drives 14 and sensors of a system of control of a power plant's thrust vectors and sensors 16 of airborne systems. The flight-navigational complex is fulfilled on the basis of unified apparatus and program-computing means providing navigation, flight control and thrust vectors of the power plant and also execution of control and evaluation of the state of the airborne systems and the aggregates of the flying vehicle in the process of exploiting.
EFFECT: increases degree of integration of the complex with airborne systems and safety of a flight of a flying vehicle; due to integration with other airborne systems the complex has lesser mass and dimensions, little expenditure of energy.
1 dwg
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Authors
Dates
2005-05-10—Published
2003-09-10—Filed