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Paul Riseborough
586e4a7d2b
|
10 years ago | |
|---|---|---|
| .. | ||
| AttErrVecMathExample | 10 years ago | |
| Common | 10 years ago | |
| GimbalEstimatorExample | 10 years ago | |
| QuaternionMathExample | 10 years ago | |
| testData | 10 years ago | |
| ReadMe.txt | 10 years ago | |
ReadMe.txt
Matlab derivations and simulations relating to development of the small EKF containing the following material:
testData: bench and flight test data used by the various estimator test harnesses
QuaternionMathExample: Small EKF using the same quaternion attitude representation as the main EKF and with a in-flight alignment test using real data. The inability to perform and in-flight alignment demonstrated by this example shows why we have change to a different attitude representation for the samll EKF.
AttErrVecExample: Small EKF using a new error vector representation for the vehicle attitude and subjected to in-flight alignment tests using both simulated and real data. The robust alignment achieved shows why this new math has been selected for use in the small EKF.
GimbalEstimatorExample: A simulation of 3 axis stabilised gimbal estimator showing application of the small EKF combined with a high rate predictor running on the gimbal that is corrected using the EKF attitude estimates.
Common: Common Matlab functions