The invention discloses an
engine power compensation
system of an air vehicle; a logarithmic circuit is used for applying a natural logarithm operation circuit to perform natural logarithm operation solving on a flow
signal and an expected flow
signal which are measured by a flow sensor and enter an air power motor separately; a division operation is carried out through a divider IC1 under the control of a synchronous switch, and a flow
signal needing to be compensated is directly obtained; the circuit structure is simple, and the calculation is accurate; a signal
coupling circuit receives a flow compensation signal and converts the flow compensation signal into a signal for driving a flow valve through a proportional amplification circuit with feedback, then the signal enters an
operational amplifier AR5 and is coupled with the fed-back flow signal, and then is subjected to amplitude limiting and filtering after
voltage stabilization, and then is output to the grid
electrode of a MOStransistor Q5; and a flow valve
driving circuit is used for carrying out primary-stage
voltage regulation on a
differential amplifier which takes an
operational amplifier AR3 as the core, and the second-stage
voltage regulation on the MOS
transistor Q5 and then driving a flow valve motor, so that the output voltage of the drain
electrode of the MOS
transistor Q5 is stable, the adjusting precisionis improved, and the problem that the closed-loop feedback
system is not timely adjusted is solved.