forked from Archive/PX4-Autopilot
10 lines
614 B
Plaintext
10 lines
614 B
Plaintext
The EKF uses a range of techniques acquired from several years of experience including an original method to handle the delayed time horizon problem.
|
|
A list of references I have found useful has been included.
|
|
|
|
- The Matlab script used to derive the autocoded expressions in the EKF can be found here: https://github.com/PX4/ecl/blob/master/EKF/matlab/scripts/Inertial%20Nav%20EKF/GenerateNavFilterEquations.m
|
|
|
|
- A working Matlab model of the filter capable of replaying flight data can be found here: https://github.com/PX4/ecl/tree/master/EKF/matlab/EKF_replay
|
|
|
|
Paul Riseborough
|
|
https://github.com/priseborough
|