Observability analysis for "Inertial Yaw-Independent Velocity and Attitude Estimation for High Speed Quadrotor Flight"
Mathematica 100.00%
observability_analysis's Introduction
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Instructions:
Please run these notebooks in Mathematica.
From that program, the files will be readable.
Don't try to read the files in a text editor.
Lines followed by semicolons are visually suppressed.
To see the output of a line, remove the semicolon and
reevaluate the file.
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The relevant works:
1) observability_analysis.nb:
Inertial Yaw-Independent Velocity and Attitude Estimation for High Speed Quadrotor Flight
2) observability_analysis_2.nb:
IMU-Based State Estimation for a Quadrotor UAV Leveraging Eulerian Dynamics (under review)
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