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  • DQRC14A
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Created with Raphaël 2.2.025Aug24232221201918171615141312109876545432131Jul3029282726252423222120Update nuttx with backport Kinetis i2c fix (#10325)camera_trigger.msg: add feedback field to understand if message camera from trigger or capture drivercamera_capture: add cycle for cycle_trampolineJenkins update CMAKE_BUILD_TYPE to PX4_CMAKE_BUILD_TYPEJenkins SITL tests add cmake build type choicefxos8701cq:Clean up & paramater based low pass fileterfxas21002c:Clean and speed up with SW, HW LPF.Doxy documentation work in px4_module_params.h and px4_module.h.WIP ITCM hackspr-itcm_hackspr-itcm_hacksFixed-wing autoland: Introduce parameter to enable/disable the early activation of the landing configurationFixed-wing autoland: Remove the dynamic altitude acceptance calculation and just use a simple separate landing altitude acceptance radius instead. This gives users that do not use LOITER-TO-ALT waypoints more control over their landing procedureFixed-wing autoland: Parameter description fixesFixed-wing autoland: Adapt according to @dagar's and @antiheavy's comments.Fixed-wing autoland: ALWAYS flare when close to the ground, independently of the horizontal distance to the land WP. This avoids that we crash into the ground at negative pitch and guarantees that the flare always starts at the same altitude above ground. However, the motor shutoff still depends on the horizontal distance to the LAND WP, thus avoiding that the motor is shut off prematurelyFixed-wing autoland: Use a more appropriate (i.e. mostly tighter) altitude acceptance radius than just the standard altitude acceptance parameter (which may be too large to allow a precise autoland)Fixed-wing autoland: 1) The landing configuration (flaps, different airspeed) is now already set during the loiter down instead of at the start of the landing approach. This is done to avoid any mode changes (which can cause altitude/airspeed jumps) so close to the gorund. 2) A scaling factor for the TECS throttle time constant was added which allows tighter throttle control during the landing (i.e. close to the ground) than high up in the airflighttask static method to check if data is availableflighttask-chec…flighttask-check-dataNXPHlite-v3:Ensure bin file sizes in mtpl of 8NXPHlite:Track kinetis upstream CONFIG changesNuttx with Missing Backportskinetis:Fixed hard fault when called with nullptr for erratarc.mavlink:Seperate sys compaion init dependant on MAVLINK_COMPANION_DEVICErc.mavlink:NXPhlite Mavlink on ttyS4 and ttyACM onlyrc.mavlink:Fix syntax errorsJenkins add separate Ubuntu 18.04 posix_sitl_default buildJenkins update cppcheck to px4-dev-base:2018-08-23 with fixed python dependenciesUpdate submodule ecl to latest Thu Aug 23 09:46:28 EDT 2018Directly set parameters in airframe config files rather than setting script variables and move the param set lines into logic blocks, and alphabetize and tidy up param set lists.mavlink: switch back from _mavlink_timesync.sync_stamp to hrt_absolute_timeclean up camera capture driveradd camera capture mode and edge paramsrename camera capture feedback param and move it from camera_feedback module to camera capture driveradd camera trigger feedback (input capture when camera actually takes the photo)Camera Capture - Use falling edge onlyCamera Capture - add "status" to camera_capture usage help messageCamera Capture - enable capture at startupCamera Capture - add module to fmu-v5 cmakeAdd camera_capture driverJenkins update cppcheck to px4io/px4-dev-base:2018-08-21 (ubuntu 18.04)navigator: add yaw setpoint to rcloss state (#10291)