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| Bob-II
overlays 28 columns x 11 rows of white text with a black border. |
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| Everything
underlined is updated; all else is static. Air sensor data and |
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| attitude
data are updated as fast as the micro-controller can process the |
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| sensor
inputs. GPS data and tachometers
are updated at 1 Hz. |
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| A XXX
mph = air data airspeed (mph) |
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| XXXXX ft = air data altitude (ft) |
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| L XXXXX
RPM = |
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| left tach (rpm) |
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| R XXXXX
RPM = |
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| right tach
(rpm) |
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| L |
| 9 |
| 9 |
| 9 |
| 9 |
| r |
| p |
| m |
| A |
| 9 |
| 9 |
| m |
| h |
| R |
| 9 |
| 9 |
| 9 |
| 9 |
| 9 |
| r |
| p |
| P |
| 0 |
| U |
| R |
| 0 |
| R |
| 9 |
| 9 |
| 9 |
| 9 |
| 9 |
| f |
| t |
| P |
| 9 |
| 0 |
| U |
| R |
| 9 |
| 0 |
| R |
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| (Analog
accelerometers) |
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| P XX
U/D = |
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| pitch
in deg, up/down |
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| R XX R/L
= |
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| roll
in deg, right/left |
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| (Nanotron
tilt sensors) |
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| P XX
U/D = |
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| pitch
in deg, up/down |
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| R XX R/L
= |
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| roll
in deg, right/left |
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| h |
| h |
| : |
| m |
| s |
| s |
| G |
| 9 |
| 9 |
| m |
| h |
| d |
| d |
| : |
| m |
| : |
| s |
| s |
| N |
| H |
| 6 |
| 0 |
| d |
| e |
| g |
| 9 |
| 9 |
| 9 |
| 9 |
| 9 |
| f |
| t |
| d |
| d |
| d |
| : |
| m |
| : |
| s |
| s |
| E |
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| hh:mm:ss
= GPS Time G XXX mph = GPS ground speed (mph) dd:mm:ss N/S =
GPS latitude |
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| HD XXX
deg = GPS heading (deg) XXXXX ft = GPS altitude (ft) ddd:mm:ss E/W
= GPS longitude |
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