公开(公告)号：US4883239A

公开(公告)日：1989-11-28

申请号：US260882

申请日：1988-10-21

Applicant: Karl-Heinz Lachmann ,  Peter Sundermeyer ,  Johann Schreier ,  Albrecht Reindler ,  Jurgen Leininger

Inventor： Karl-Heinz Lachmann ,  Peter Sundermeyer ,  Johann Schreier ,  Albrecht Reindler ,  Jurgen Leininger

IPC: F41G7/00 ,  F41G7/34

CPC classification number: F41G7/008 ,  F41G7/34

Abstract: A guided artillery projectile with a flight attitude or trajectory regulator in the autopilot of the projectile for the guidance of a transition into a gliding trajectory at the assumption of a predetermined pitch angle after the passage through the apogee of the ballistic firing trajectory.

Abstract translation: 一种在射弹自动驾驶仪中具有飞行姿态或轨迹调节器的导弹炮弹，用于在通过弹道射击轨迹的远地点之后以预定的俯仰角度假设转向滑翔轨迹。

公开(公告)号：US4856733A

公开(公告)日：1989-08-15

申请号：US191588

申请日：1988-05-09

Applicant: Karl-Heinz Lachmann

Inventor： Karl-Heinz Lachmann

IPC: F41G7/00 ,  F41G7/34

CPC classification number: F41G7/343 ,  F41G7/008

Abstract: A method for the on board determination for the passage through an apogee by a ballistically launched projectile through the receipt and comparison of a sequence of measured values vacillating or fluctuating specifically relative to the trajectory. Also disclosed is an arrangement for the on board determination of the point in time of an apogee of a projectile which is launched in a ballistic trajectory, through the receipt and comparison of a sequence of measured values vacillating specific to the trajectory.

Abstract translation: 一种用于船上确定通过弹道发射的射弹通过远地点通过接收和比较相对于轨迹具体摆动或波动的测量值序列的方法。 还公开了一种用于船上确定在弹道轨迹中发射的射弹的远地点的时间点的布置，通过接收和比较特定于轨迹的一系列测量值。