发明名称 |
GUN-LAUNCHED GLIDE VEHICLE WITH A MID-COURSE AND TERMINAL GUIDANCE CONTROL SYSTEM |
摘要 |
The system comprises an eight-inch full-bore glide vehicle having retractable aerodynamic lifting surfaces which increase range performance and accuracy. The glide vehicle can be fired to a maximum range of 135 miles without guidance or to a range of 100 miles with accurate terminal guidance. An infrared horizon scanner provides feedback information to small bang-bang servo-operated roll-tabs for vehicle despin and roll-attitude stabilization. Target acquisition occurs from the glide path with ship-based radar providing information for mid-course lateral guidance control. A forward observer illuminates the target with laser energy and the vehicle homes in on the target using bang-bang monoplane control.
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申请公布号 |
US3695555(A) |
申请公布日期 |
1972.10.03 |
申请号 |
USD3695555 |
申请日期 |
1970.06.12 |
申请人 |
NAVY USA |
发明人 |
WILLIAM R. CHADWICK |
分类号 |
F41G7/22;(IPC1-7):F41G7/14;F41G7/06 |
主分类号 |
F41G7/22 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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