FIELD: aviation.
SUBSTANCE: control system in the longitudinal channel of manned and unmanned aircrafts contains a low-altitude radio altimeter, an air data system, non-platform inertial navigation system consisting of a normal overload sensor, angular pitch velocity sensor and a pilot handle position sensor, a digital path control system and a modal remote-control system, an electro-hydraulic drive. The modal remote-control system contains a unit for generation of a reduced lift coefficient, a calculator for the desired transfer function using the Schomber-Gertsen criterion, and a calculator for an astatic residual formation. The path control system contains a height control calculator and an algorithm calculator for generating a dangerous height signal.
EFFECT: provides traffic stability and flight safety when performing a dive manoeuvre in a creeping mode from a dangerous altitude.
7 dwg
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Authors
Dates
2018-02-07—Published
2016-02-12—Filed