发明名称 |
Aircraft flight data recorder data acquisition system |
摘要 |
A data acquisition system for use in an aircraft flight data recorder receives multiple analog and discrete signals representative of various aircraft parameters. A single address command from the flight data recorder central processing unit (CPU) causes a first multiplexer to select a set of analog signals. Each selected analog signal is amplified by a gain factor under CPU control and passed to track-and-hold circuitry which holds a level of the amplified analog signal upon receipt of a suitable command. The held analog signal levels are passed to a second multiplexer which also receives a set of discrete signals selected by a third multiplexer in response to a CPU address command. A control sequencer sequentially passes each signal at the input of the second multiplexer through an analog-to-digital converter, with the resultant digital signal being loaded into memory. After either all the selected and processed analog signals or the selected discrete signals have been analog-to-digital converted and stored in memory, the control sequencer issues an interrupt signal to the CPU.
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申请公布号 |
US4656585(A) |
申请公布日期 |
1987.04.07 |
申请号 |
US19840576538 |
申请日期 |
1984.02.03 |
申请人 |
SUNDSTRAND DATA CONTROL INC. |
发明人 |
STEPHENSON, EDWARD A. |
分类号 |
G01C21/00;G01D9/00;G06F3/05;G06F17/00;G06F17/40;(IPC1-7):G06F15/20 |
主分类号 |
G01C21/00 |
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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