FIELD: equipment of aircraft ejection seats. SUBSTANCE: control system includes parameter sensors, control unit and ejection seat stabilization circuit; control system is additionally provided with wind disturbance compensation circuit with wind velocity component sensor, compensation signal forming unit and compensation signal connecting unit. Proposed control system is effective at initial stage of ejection for quick spatial separation of ejection seat and carrier. EFFECT: enhanced safety of rescue ejection. 2 dwg
Title | Year | Author | Number |
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Authors
Dates
2000-05-27—Published
1999-03-03—Filed