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Tree: a74b7ef60b

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my1.12-iic

pr-sensor-distance

release/1.12

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tf-1.12

tf-1.12-print_test

tf-iic2uart

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px4_autopilot/EKF/tests/pytest

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
..
CMakeLists.txt	EKF pytest save plots to pdf	7 years ago
ekf_test.py	fix and re-enable EKF pytests	7 years ago
lint.py	fix and re-enable EKF pytests	7 years ago
plot_utils.py	EKF pytest save plots to pdf	7 years ago
requirements.txt	EKF pytest save plots to pdf	7 years ago
test_altitude.py	fix and re-enable EKF pytests	7 years ago
test_basics.py	ekf run output predictor immediately with new IMU data (#471)	7 years ago
test_sampling.py	fix and re-enable EKF pytests	7 years ago
test_utils.py	fix and re-enable EKF pytests	7 years ago