- Dec 13, 2016
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Paul Riseborough authored
Use reporting from the motor mixer to only restrict integrator growth when it will result in increased saturation of the control axis concerned. Enable absolute integrator limits to be set by parameter
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Paul Riseborough authored
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Paul Riseborough authored
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Lorenz Meier authored
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- Dec 12, 2016
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Lorenz Meier authored
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Lorenz Meier authored
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Matthias Grob authored
argv[1] was read even if argc < 2 -> segmentation fault when running without arguments the return saves this
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- Dec 11, 2016
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Julian Oes authored
According to https://github.com/mavlink/mavlink/pull/629 the mavlink command DO_SET_MODE should only determine the mode but not the armed/disarmed state, so the MAV_MODE_FLAG_SAFETY_ARMED bit should be ignored. Instead the mavlink command COMPONENT_ARM_DISARM should be used instead. Therefore, the commander now ignores the arm/disarm bit.
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Dennis Shtatnov authored
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Dennis Shtatnov authored
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- Dec 10, 2016
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Lorenz Meier authored
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Bart Slinger authored
fix code style
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Mark Whitehorn authored
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Mark Whitehorn authored
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Mark Whitehorn authored
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Mark Whitehorn authored
note that FMU does not update AUX pwm outputs if no RC signal
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Mark Whitehorn authored
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Mark Whitehorn authored
clamp mixer output offset to [-.2,.2] ([-2000, 2000] in mixer file) add 8 main PWM trim parameters add long desc to parameters and bump minor parameter version
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Bartosz Wawrzacz authored
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Anton Matosov authored
This also adds a ZMR250 config.
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- Dec 09, 2016
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Andreas Antener authored
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Andreas Antener authored
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Andreas Antener authored
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Andreas Antener authored
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Andreas Antener authored
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Andreas Antener authored
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Andreas Antener authored
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Paul Riseborough authored
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- Dec 08, 2016
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Julian Oes authored
This fixes the following corner case: 1. Upload a mission. 2. Set mission mode. 3. Set loiter mode. 4. Arm. At this point it will shoot up and go to the takeoff waypoint even though we're not in mission but in loiter mode. The fix makes sure that the triplet is reset to invalid (and idle) in loiter mode if we're landed and disarmed. It will lead to the vehcle sit in idle on the ground until you issue a start mission (or takeoff) command.
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Dennis Mannhart authored
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Dennis Mannhart authored
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Roman authored
- fix a bug where the wrong rotation order was used to compute the attitude setpoint when using the pusher assist feature Signed-off-by:
Roman <bapstroman@gmail.com>
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- Dec 07, 2016
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Dennis Mannhart authored
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Dennis Mannhart authored
- Dec 06, 2016
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James Goppert authored
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- Dec 05, 2016
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Roman authored
- fixed a bug where tilt compensation was done also when the horizontal velocity was controlled. This is not needed because in this case the controller outputs a 3D thrust vector. Signed-off-by:
Roman <bapstroman@gmail.com>
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Daniel Agar authored
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Daniel Agar authored
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Lorenz Meier authored
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