| 摘要 |
FIELD: aircraft engineering.SUBSTANCE: this complex comprises onboard system of flight parameters measurement, computer, input signal normalizing unit, tunable generator of audio codes, unit for selection and adjustment of input signal parameters and unit for harmonizing and auding of parameters. Said computer comprises ADC, sound code generator, load speaker or headphones. ADC, input signal normalizing unit and sound code generator are connected in series. Input signal normalizing unit is connected with for selection and adjustment of input signal parameters and unit for harmonizing and auding of parameters. Switch P1 is connected with sound code generator sound digital characteristics generator. Selection and adjustment unit is connected with adjustment unit panel. Harmonizing unit is connected via switch P2 with memory units with settings connected via switch P3 with the sound digital characteristics generator unit.EFFECT: pilot info support with the help of musical interpretation of flight parameters.3 dwg |
