发明名称 |
GLIDBANEVARNINGSINSTUMENT FOR FLYGFARKOST |
摘要 |
In a system where the aircraft's distance below a radio glide slope is compared with the aircraft's altitude above ground to generate either an advisory voice warning or a command voice warning depending upon the aircraft's altitude and distance below the radial glide slope beam, the repetition rate of the advisory voice warning is varied as both a function of distance below the radio glide slope beam and of altitude in order to generate advisory warnings at a rate reflecting increasing danger to the aircraft. This is accomplished by integrating the glide slope deviation signal over time and comparing it with a radio altitude signal so as to generate a signal for triggering the advisory warning as a function of the glide slope deviation and the radio altitude thereby generating the advisory warnings as a function of decreasing radio altitude and increasing deviation from the glide slope. |
申请公布号 |
SE416034(B) |
申请公布日期 |
1980.11.24 |
申请号 |
SE19760003426 |
申请日期 |
1976.03.19 |
申请人 |
* SUNDSTRAND DATA CONTORL INC |
发明人 |
C D * BATEMAN;H R * MULLER |
分类号 |
B64D45/04;G01C5/00;G01S1/02;G01S19/14;G01S19/49;G05D1/06;(IPC1-7):64D45/04;05D1/04 |
主分类号 |
B64D45/04 |
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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