- Nov 07, 2014
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Randy Mackay authored
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- Oct 31, 2014
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Randy Mackay authored
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- Oct 29, 2014
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Randy Mackay authored
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priseborough authored
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Randy Mackay authored
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Randy Mackay authored
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Randy Mackay authored
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priseborough authored
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priseborough authored
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Randy Mackay authored
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Benoit PEREIRA DA SILVA authored
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Randy Mackay authored
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Randy Mackay authored
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Jonathan Challinger authored
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- Oct 27, 2014
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Randy Mackay authored
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Randy Mackay authored
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Andrew Tridgell authored
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Randy Mackay authored
dcm-check was triggering after 10 bad headings but these did not need to be continuous meaning if the vehicle was flown long enough it would almost certainly trigger a dcm-check failure and land
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- Oct 24, 2014
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Randy Mackay authored
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Andrew Tridgell authored
this allows the range of the Lidar to be set by the user using RNGFND_MAX_CM and RNGFND_MIN_CM
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- Oct 23, 2014
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Randy Mackay authored
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Randy Mackay authored
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Randy Mackay authored
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Randy Mackay authored
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Randy Mackay authored
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Randy Mackay authored
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Randy Mackay authored
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Randy Mackay authored
The functions in the mount lib didn't work anyway
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Randy Mackay authored
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- Oct 22, 2014
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Randy Mackay authored
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Randy Mackay authored
Barometer climb rate must be -150cm/s ~ +150cm/s This threshold is generous because we already use the inertial navigation climb rate so this is just to catch cases where inertial nav is very incorrect in it's climbrate estimates
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Jonathan Challinger authored
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- Oct 21, 2014
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Randy Mackay authored
This corrects a bug that allowed the waypoint speed to be set to zero
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Randy Mackay authored
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Randy Mackay authored
fixes issue in which now could be earlier than _last_update_xy_ms leading to a large dt value and a sudden lean on takeoff
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- Oct 20, 2014
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priseborough authored
This will help prevent spurious alt disparity warning messages for copter
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Randy Mackay authored
Issue discovered and fix contributed by Deadolous
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- Oct 18, 2014
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Randy Mackay authored
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Randy Mackay authored
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Randy Mackay authored
This resolves the issue of the parachute servo's position not being initialised to the off position due to an ordering problem of the auxiliary servos being initialised after the parachute object.
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