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Tree: a74b7ef60b

main

master

my1.12

my1.12-iic

pr-sensor-distance

release/1.12

sbg

tf-1.12

tf-1.12-print_test

tf-iic2uart

tf_driver-1.12

tf_i2c-1.12

tf_i2c_collis_pre

v1.13.0-BW

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px4_autopilot/EKF/tests

History

Daniel Agar cebdc3d829 ekf run output predictor immediately with new IMU data (#471) ... * EKF collect_imu take const imu sample and populate buffer * EKF calculateOutputStates cleanup * EKF add calculate_quaternion output predictor method * EKF: update documentation * EKF: remove unnecessary getter function * EKF calculateOutputStates only apply dt correction to bias * EKF pytest assert attitude validity, not update() return * EKF: correct documentation * EKF: Do not make attitude validity dependent on yaw alignment status Yaw alignment could fail in flight due to temporary loss of data and yet the quaternions would still usable for stabilisation even though the absolute earth yaw angle wrt true north was uncertain.		7 years ago
..
base	cmake and Jenkins add basic address santiizer test buld	7 years ago
pytest	ekf run output predictor immediately with new IMU data (#471)	7 years ago
ringbuffer	fix and re-enable EKF pytests	7 years ago
CMakeLists.txt	code coverage cmake and Jenkins support	7 years ago