A multi-redundancy, full-function and aviation-grade flight control and navigation system with 3 independent flight control units.
SPECIFICATIONS
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SPECIFICATIONS |
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Processor |
MPC5200B |
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GPS |
10Hz, positioning accuracy 2.5m |
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3 axis gyroscopes |
±300deg/s (±450deg/s for choice) |
|
3 axis accelerator |
±18g |
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3 axis magnetic sensor |
±8G |
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Static pressure sensor |
103.35kPa， height resolution0.1m |
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Dynamic pressure sensor |
13.78kPa，support 540km/h |
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Analogue input |
6 channels, 16BitAnalogue |
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Communication interface |
6 channels, RS232/RS422/RS485 for choiceCommunication |
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BDS/DGPS module |
20Hz,RTK positioning accuracy 1cm + 1ppm |
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Digital signal input |
10 channels PWM or general I/O |
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Digital signal output |
24 channels PWM or general I/O |
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Power input |
2channels |
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ElECTRIC SPECS |
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Power supply |
DC8～30V |
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Power consumption |
＜10W |
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PHYSICAL SPECS |
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Size |
182×166×100mm |
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Weight |
3500g |
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OPERATING ENVIRONMENT |
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Storage temperature |
-55ºC ~ +85ºC |
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Storage humidity |
5% ~ 95% |
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Operating temperature |
-40ºC ~ +70ºC（Calibrated range, no case） |
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Operating humidity |
10% ~ 90% |