发明名称 Guided artillery projectile with trajectory regulator
摘要 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.
申请公布号 US4883239(A) 申请公布日期 1989.11.28
申请号 US19880260882 申请日期 1988.10.21
申请人 DIEHL GMBH & CO. 发明人 LACHMANN, KARL-HEINZ;SUNDERMEYER, PETER;SCHREIER, JOHANN;REINDLER, ALBRECHT;LEININGER, JURGEN
分类号 F41G7/00;F41G7/34 主分类号 F41G7/00
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