GitHub - avani-p/AE4320_SystemIdentification: Assignment Submission for the System Identification of Aerospace Vehicle (AE4320) course. Two Step Approach to Identify Aerodynamic Model - State Estimation and Parameter Estimation

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Assignment Submission for the System Identification of Aerospace Vehicle (AE4320) course. Two Step Approach to Identify Aerodynamic Model - State Estimation and Parameter Estimation

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Name		Name	Last commit message	Last commit date
Latest commit History 4 Commits
simdata2023		simdata2023
Assignment_01_StateEst.m		Assignment_01_StateEst.m
Assignment_02_ParamEst.m		Assignment_02_ParamEst.m
IterativeExtendedKF.m		IterativeExtendedKF.m
ParamEst_OLS.m		ParamEst_OLS.m
ParamEst_RLS.m		ParamEst_RLS.m
PlotAerodynamicModel.m		PlotAerodynamicModel.m
PlotBiases.m		PlotBiases.m
PlotError.m		PlotError.m
PlotParamComparison.m		PlotParamComparison.m
PlotResidual.m		PlotResidual.m
PlotStates.m		PlotStates.m
PlotVariances.m		PlotVariances.m
body2ned.m		body2ned.m
jacobian_matrices.m		jacobian_matrices.m
kf_calc_ObsRank.m		kf_calc_ObsRank.m
kf_calc_jacobian.m		kf_calc_jacobian.m
kf_sys_dynamics.m		kf_sys_dynamics.m
ned2body.m		ned2body.m

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Assignment Submission for the System Identification of Aerospace Vehicle (AE4320) course. Two Step Approach to Identify Aerodynamic Model - State Estimation and Parameter Estimation

validation parameter-estimation system-identification kalman-filter aerodynamic-analysis

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