发明授权
- 专利标题： Variable gravity bias control system for a guided missile
- 专利标题（中）： 导弹可变重力偏置控制系统
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申请号： US06290747申请日： 1981-07-30
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公开(公告)号： US06578791B1公开(公告)日： 2003-06-17
- 发明人: Everett K. Jenne , H. Lowell Smith
- 申请人： Everett K. Jenne , H. Lowell Smith
- 主分类号： F41G722
- IPC分类号： F41G722
摘要：
A missile flight control initiating device for optimizing flight control time and a variable gravity bias device that corrects guidance signals from the missile's guidance computer during the optimized flight control time. These devices function to correct for the droop in trajectory caused by gravity so that the missile passes above the target.
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