| 摘要 |
FIELD: aviation. ^ SUBSTANCE: airplane and helicopter (below - aircraft) integrated standby equipment system designed as independent assembly contains liquid-crystal display, total and static pressure probes pipeline connected to onboard total and static pressure probes, electronic calculators of total and static pressure, spatial orientation module with off-line inertial sensors calculating aircraft spatial position (pitch angle, list angle), electronic calculator of indicated airspeed, barometric height, vertical speed and number M, satellite navigator and onboard navigation system "" data receivers, onboard magnetic probe data receivers, radio facilities data receivers and braking temperature receiver, engine control system data receivers, spatial position and course calculators considering correction under satellite navigation system and "" data, course calculators with correction under magnetic probe and radio facilities data, and electronic signal converter to required shape and displaying on liquid-crystal display and onboard systems. ^ EFFECT: higher accuracy of calculated flight-navigating parameters, higher data volume on liquid-crystal display. ^ 6 cl, 1 dwg |
