| 摘要 |
Flight control system for a rotary-wing aircraft, particularly for a helicopter.The flight control system comprises at least one flight control (LCo, MCy, Pal), first commands being representative of the position of a flight control (LCo, MCy, Pal), an assisted flight control system (CDVE) generating assistance values representing second commands, first unit (CDVE) for determining the control commands from the sum of the first and second commands, and a limitation system (SL) which limits the assistance values to first limited values. This limitation system (SL) additionally comprises unit for calculating the difference between the assistance values and the first limited values, and unit for calculating the sum of the first limited values and of difference and for transmitting it as second commands.
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