发明名称 |
Aircraft launched missile system that has built in controller for reconfiguration and allows function monitoring and error detection |
摘要 |
The airborne guided missile is coupled to the launch aircraft by a data link and a starter unit. The missile has an electronic system that consists of hardware and software and has function monitoring, error detection and allows reconfiguration to be made. The monitoring system is model based and includes redundancy functions.
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申请公布号 |
DE19857894(A1) |
申请公布日期 |
2000.06.21 |
申请号 |
DE19981057894 |
申请日期 |
1998.12.15 |
申请人 |
BODENSEEWERK GERAETETECHNIK GMBH |
发明人 |
KROGMANN, UWE |
分类号 |
F41G7/22;(IPC1-7):F42B15/01;F41G7/00;G05B13/02 |
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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