EJECTION SEAT CONTROL SYSTEM FOR RESCUE OF CREW

FIELD: ejection means for rescue of crew. SUBSTANCE: control system includes state parameter sensor unit, difference unit, ejection seat stabilization circuit and preset trajectory forming unit which are connected in series. Control system is additionally provided with correcting filter and complex...

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Bibliographische Detailangaben
Hauptverfasser:	DZHANDZHGAVA G.I, BAKHONIN K.A, FEDULOV N.P, EFANOV A.A, JAKOVLEV N.N, LIVSHITS A.N, MJAKISHEV G.A, NEGRIKOV V.V, SEVERIN G.I, BUDKIN V.L
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	FIELD: ejection means for rescue of crew. SUBSTANCE: control system includes state parameter sensor unit, difference unit, ejection seat stabilization circuit and preset trajectory forming unit which are connected in series. Control system is additionally provided with correcting filter and complex signal shaping unit to ensure optimal quality of control and accurate tracking of preset space and time trajectories. EFFECT: safety of rescue of crew members; enhanced efficiency of ejection. 2 dwg