Qrot {RSpincalc} | R Documentation |
Qrot
updates the current attitude quaternion.
Qrot(Q, w, dT)
Q |
Quaternion (Q) vector [q1, q2, q3, q4]. |
w |
Angular rate values [wx, wy, wz]. |
dT |
Inverse of update rate. |
Q |
Updated quaternion (Q) vector [q1, q2, q3, q4]. |
Jose Gama
Q <- c(-0.1677489, -0.7369231, -0.3682588, 0.5414703)
w <- c(0.1, 0.2, 0.3)
dT <- -.12
Qrot(Q,w,dT)