FIELD: aviation.
SUBSTANCE: in the event of malfunction of command pressure indicators, a command for the execution of the backup control algorithm for the ramjet engine is issued. The predetermined height of the winged rocket is reached and the speed of the winged rocket is maintained, corresponding to the altitude of the flight of the winged rocket. At the same time, the fuel consumption is regulated by the speed and altitude parameters of the winged rocket, and the height and speed of the winged rocket are measured using satellite navigation equipment.
EFFECT: increase of reliability of work and increase of survivability and safety of flight.
2 cl, 1 dwg
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