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DEVICE MANAGEMENT SYSTEM WORK navigation control in a mode with reduced functionality

机译:设备管理系统在功能降低的模式下进行导航控制

摘要

1. System operation control device (40) navigation control, and navigation control device is adapted to control the immersion depth and / or lateral position of a towed linear acoustic antenna (20a) and comprises a body (11) to which is attached a set of wings, comprising: means ( 55, 91) for operation of the navigation control unit in a reduced functionality mode by acting on at least one wing, not unconnected and provided with a driven elektrodv igatelya, when detecting that at least one wing of said set of wings to be disconnected or otsoedineno.2. Control system according to claim 1, characterized in that said means for operating comprises: -. schema (55, 91) deciding the loss of the wing for generating wing loss signal when detecting that at least one wing of said set wings disconnected or must be disconnected; u circuit (55), the control that is part of the navigation control device for controlling the navigation control apparatus in accordance with the mode with reduced functionality when receiving said wing loss signal, said reduced operating mode enables control at least the depth immersing a towed linear acoustic antenny.3. Control system according to claim. 2, characterized in that said at least one wing that is disconnected or must be disconnected, contains an embedded magnet, said operation control system comprises magn
机译:1.系统操作控制装置(40)的导航控制,并且该导航控制装置适于控制被牵引的线性声波天线(20a)的浸入深度和/或横向位置,并且包括附有一组的主体(11)。机翼,包括:装置(55、91),用于在检测到所述至少一个机翼的至少一个机翼时,通过作用于至少一个未连接并且配备有从动天线的机翼,以减小的功能模式操作导航控制单元。一组要断开的机翼或otsoedineno.2。 2.根据权利要求1所述的控制系统,其特征在于,所述用于操作的装置包括:-。模式(55、91),当检测到所述机翼中的至少一个机翼已断开或必须断开时,确定用于产生机翼损失信号的机翼的损失;在电路(55)中,该控制是导航控制装置的一部分,用于在接收到所述机翼损失信号时根据具有减小的功能的模式来控制导航控制装置,所述减小的操作模式使得能够至少控制沉入被拖曳物的深度线性声学天线3。根据权利要求的控制系统。参照图2,其特征在于,所述至少一个已断开或必须断开的机翼包含嵌入式磁体,所述操作控制系统包括magn

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