research
          
      
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      08/06/2022
    Log-linear Error State Model Derivation without Approximation for INS
Through assembling the navigation parameters as matrix Lie group state, ...
          
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      10/26/2021
    MEKF Ignoring Initial Conditions for Attitude Estimation Using Vector Observations
In this paper, the well-known multiplicative extended Kalman filter (MEK...
          
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      03/03/2021
    Inertial based Integration with Transformed INS Mechanization in Earth Frame
This paper proposes to use a newly-derived transformed inertial navigati...
          
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      02/25/2021
    Strapdown Inertial Navigation System Initial Alignment based on Group of Double Direct Spatial Isometries
The task of strapdown inertial navigation system (SINS) initial alignmen...
          
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      03/29/2020
    SE(3) based Extended Kalman Filter for Spacecraft Attitude Estimation
In this paper, the spacecraft attitude estimation problem has been inves...
          
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      01/16/2018
    Semi-Analytic Method for SINS Attitude and Parameters Online Estimation
In this note, the attitude and inertial sensors drift biases estimation ...
          
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      10/11/2017
     
             
  
  
     
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