Bilag 1: Helikopterens fysiske egenskaber - SmartData
Bilag 1: Helikopterens fysiske egenskaber - SmartData
Bilag 1: Helikopterens fysiske egenskaber - SmartData
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Attitude estimation library<br />
Detailed Description<br />
AccAHRS.h<br />
3<br />
<strong>Bilag</strong> 12: Anvendte C++ programmer<br />
Attitude & Heading Ref. System based on accelerometer input ONLY<br />
Attitude.h Contains functions for converting between different attitude representations.<br />
Note:<br />
Most of the functions in here are tightly coupled to the definitions of the<br />
helicopter- & navigation-frames (or references if you like), and the rotationorder<br />
of the Euler angles. Currently the used rotation-order for transforming<br />
from the helicopter-frame to the navigation-frame is Yaw-Pitch-Roll<br />
GyroAHRS.h<br />
Attitude & Heading Ref. System based on gyro input ONLY<br />
KalmanAHRS.v1.h Attitude & Heading Ref. System based on Kalman filtering of<br />
BOTH accelerometer & Gyro inputs<br />
Classes<br />
Typedefs<br />
class AccAHRS<br />
class GyroAHRS<br />
class KalmanAHRS_v1<br />
class KalmanAHRS_v1<br />
typedef KalmanAHRS_v1 KalmanAHRS
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