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derivation
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AP_NavEKF3: Use alternate form for quaternion to rotmat equations in derivation
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2021-07-23 10:19:49 +09:00 |
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AP_NavEKF3.cpp
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AP_NavEKF3: Add accessor function for vibration affected status
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2021-07-23 10:19:50 +09:00 |
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AP_NavEKF3.h
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AP_NavEKF3: Add accessor function for vibration affected status
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2021-07-23 10:19:50 +09:00 |
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AP_NavEKF3_AirDataFusion.cpp
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AP_NavEKF3: convert powF(xx,2) calls to sq(xx)
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2021-07-23 10:19:46 +09:00 |
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AP_NavEKF3_Control.cpp
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AP_NavEKF3: implement moving origin
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2021-07-23 10:19:46 +09:00 |
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AP_NavEKF3_GyroBias.cpp
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AP_NavEKF3: allow for double EKF build
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2021-07-23 10:19:46 +09:00 |
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AP_NavEKF3_Logging.cpp
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AP_NavEKF3: allow for double EKF build
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2021-07-23 10:19:46 +09:00 |
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AP_NavEKF3_MagFusion.cpp
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AP_NavEKF3: allow for double EKF build
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2021-07-23 10:19:46 +09:00 |
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AP_NavEKF3_Measurements.cpp
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AP_NavEKF3: process GPS yaw independently of GPS fix
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2021-07-23 10:19:46 +09:00 |
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AP_NavEKF3_OptFlowFusion.cpp
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AP_NavEKF3: Don't update accel bias states if vibration affected
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2021-07-23 10:19:50 +09:00 |
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AP_NavEKF3_Outputs.cpp
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AP_NavEKF3: pass NavEKF failures back up to callers
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2021-07-23 10:19:46 +09:00 |
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AP_NavEKF3_PosVelFusion.cpp
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AP_NAvEKF3: use #define value for bad IMU hold time
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2021-07-23 10:19:50 +09:00 |
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AP_NavEKF3_RngBcnFusion.cpp
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AP_NavEKF3: Don't update accel bias states if vibration affected
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2021-07-23 10:19:50 +09:00 |
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AP_NavEKF3_VehicleStatus.cpp
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AP_NavEKF3: allow for double EKF build
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2021-07-23 10:19:46 +09:00 |
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AP_NavEKF3_core.cpp
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AP_NavEKF3: Increase lower state variance limit when vibration affected
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2021-07-23 10:19:50 +09:00 |
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AP_NavEKF3_core.h
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AP_NAvEKF3: use #define value for bad IMU hold time
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2021-07-23 10:19:50 +09:00 |
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AP_NavEKF3_feature.h
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AP_NavEKF3: make drag fusion optional
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2021-01-24 11:56:52 +11:00 |
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LogStructure.h
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AP_NavEKF3: Update log message format description
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2021-03-23 10:05:59 +11:00 |
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