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cd2ca57ec2ff8e5c3ecb8116dd827044f836b1de
PX4-Autopilot/matlab/scripts/Inertial Nav EKF
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Paul Riseborough 9cf0948bcf matlab: add derivation for air data error equations
2017-08-12 20:59:41 +10:00
..
Airspeed.mat
EKF: update derivation files
2016-05-05 21:23:03 +10:00
C_code24.txt
EKF: update derivation files
2016-05-05 21:23:03 +10:00
calcH_YAW312.c
EKF: update derivation files
2016-05-05 21:23:03 +10:00
calcH_YAW321.c
EKF: update derivation files
2016-05-05 21:23:03 +10:00
calcMAGD.c
EKF: Include all output files generated by derivation script
2016-04-05 22:23:37 +02:00
ConvertToC.m
EKF: Update derivation scripts and outputs
2016-03-11 11:03:43 +11:00
ConvertToM.m
EKF: Update derivation scripts and outputs
2016-03-11 11:03:43 +11:00
derive_air_data_errors.m
matlab: add derivation for air data error equations
2017-08-12 20:59:41 +10:00
Drag.mat
EKF: update derivation files
2016-05-05 21:23:03 +10:00
EulToQuat.m
Add derivation script files for inertial nav EKF
2015-11-03 12:24:43 +11:00
fix_c_code.m
EKF: Update derivation scripts and outputs
2016-03-11 11:03:43 +11:00
GenerateNavFilterEquations.m
Matlab: Improve efficiency of odometry derivation
2017-06-03 12:39:24 +10:00
H_LOSX.c
EKF: update derivation files
2016-05-05 21:23:03 +10:00
H_LOSY.c
EKF: update derivation files
2016-05-05 21:23:03 +10:00
H_VELX.c
EKF: Clean up auto-code files for body frame velocity measurements
2017-03-06 09:01:46 +11:00
H_VELY.c
EKF: Clean up auto-code files for body frame velocity measurements
2017-03-06 09:01:46 +11:00
H_VELZ.c
EKF: Clean up auto-code files for body frame velocity measurements
2017-03-06 09:01:46 +11:00
K_LOSX.c
EKF: update derivation files
2016-05-05 21:23:03 +10:00
K_LOSY.c
EKF: update derivation files
2016-05-05 21:23:03 +10:00
K_VELX.c
EKF: Clean up auto-code files for body frame velocity measurements
2017-03-06 09:01:46 +11:00
K_VELY.c
EKF: Clean up auto-code files for body frame velocity measurements
2017-03-06 09:01:46 +11:00
K_VELZ.c
EKF: Clean up auto-code files for body frame velocity measurements
2017-03-06 09:01:46 +11:00
M_code24.txt
EKF: update derivation files
2016-05-05 21:23:03 +10:00
Magnetometer.mat
EKF: update derivation files
2016-05-05 21:23:03 +10:00
NormQuat.m
Add derivation script files for inertial nav EKF
2015-11-03 12:24:43 +11:00
OptimiseAlgebra.m
Add derivation script files for inertial nav EKF
2015-11-03 12:24:43 +11:00
polar2cart_cov.m
scripts: derive conversion from polar to cartesian wind state covariance
2016-08-11 15:26:21 +02:00
Q_airdata.c
matlab: add derivation for air data error equations
2017-08-12 20:59:41 +10:00
quat2yaw312.m
matlab: Allow replay to handle late start GPS data in log
2017-07-24 16:34:50 +10:00
quat2yaw321.m
matlab: Fix derivation for 321 Euler rotation sequence
2017-07-21 10:48:54 +10:00
Quat2Tbn.m
Add derivation script files for inertial nav EKF
2015-11-03 12:24:43 +11:00
quatCovMat.c
EKF: derive auto-code for quaternion state covariance initialisation
2016-05-17 12:28:58 +10:00
QuatDivide.m
Add derivation script files for inertial nav EKF
2015-11-03 12:24:43 +11:00
QuatErrTransferEquations.m
EKF: derive auto-code for quaternion state covariance initialisation
2016-05-17 12:28:58 +10:00
QuatMult.m
Add derivation script files for inertial nav EKF
2015-11-03 12:24:43 +11:00
QuatToEul.m
Add derivation script files for inertial nav EKF
2015-11-03 12:24:43 +11:00
RotToQuat.m
Add derivation script files for inertial nav EKF
2015-11-03 12:24:43 +11:00
rotVarVec.c
EKF: Add matlab derivation for calculation of rotation vector variance
2016-05-17 10:56:19 +10:00
SaveScriptCode.m
EKF: Update derivation scripts and outputs
2016-03-11 11:03:43 +11:00
Sideslip.mat
EKF: update derivation files
2016-05-05 21:23:03 +10:00
StateAndCovariancePrediction.mat
EKF: update derivation files
2016-05-05 21:23:03 +10:00
StatePrediction.mat
EKF: update derivation files
2016-05-05 21:23:03 +10:00
SymbolicOutput24.mat
EKF: update derivation files
2016-05-05 21:23:03 +10:00
SymbolicOutput24.txt
EKF: update derivation files
2016-05-05 21:23:03 +10:00
Tbn_312.c
matlab: Add scripts to calculate rotation conversions for 321 or 312 Euler sequences
2017-07-21 10:22:17 +10:00
Tbn_321.c
matlab: Add scripts to calculate rotation conversions for 321 or 312 Euler sequences
2017-07-21 10:22:17 +10:00
Tbn_quat.c
matlab: Add scripts to calculate rotation conversions for 321 or 312 Euler sequences
2017-07-21 10:22:17 +10:00
temp1.mat
EKF: update derivation files
2016-05-05 21:23:03 +10:00
temp2.mat
EKF: update derivation files
2016-05-05 21:23:03 +10:00
temp3.mat
EKF: update derivation files
2016-05-05 21:23:03 +10:00
test_output_filter_gains.m
EKF: add matlab script to test complementary filter gains
2016-04-30 11:05:03 +10:00
yaw_input_312.c
matlab: Add scripts to calculate rotation conversions for 321 or 312 Euler sequences
2017-07-21 10:22:17 +10:00
yaw_input_321.c
matlab: Fix derivation for 321 Euler rotation sequence
2017-07-21 10:48:54 +10:00