RWConfigLogMsgPayload
-
struct RWConfigLogMsgPayload
- #include <RWConfigLogMsgPayload.h>
Structure used to define the individual RW configuration data message.
Public Members
-
double rWB_B[3]
[m], position vector of the RW relative to the spacecraft body frame
-
double gsHat_B[3]
[-] spin axis unit vector in body frame
-
double w2Hat0_B[3]
[-] initial torque axis unit vector in body frame
-
double w3Hat0_B[3]
[-] initial gimbal axis unit vector in body frame
-
double mass
[kg], reaction wheel rotor mass
-
double theta
[rad], wheel angle
-
double Omega
[rad/s], wheel speed
-
double Js
[kg-m^2], spin axis gsHat rotor moment of inertia
-
double Jt
[kg-m^2], gtHat axis rotor moment of inertia
-
double Jg
[kg-m^2], ggHat axis rotor moment of inertia
-
double U_s
[kg-m], static imbalance
-
double U_d
[kg-m^2], dynamic imbalance
-
double d
[m], wheel center of mass offset from wheel frame origin
-
double J13
[kg-m^2], x-z inertia of wheel about wheel center in wheel frame (imbalance)
-
double u_current
[N-m], current motor torque
-
double frictionTorque
[N-m], friction Torque
-
double u_max
[N-m], Max torque
-
double u_min
[N-m], Min torque
-
double u_f
[N-m], Coulomb friction torque magnitude
-
double Omega_max
[rad/s], max wheel speed
-
double P_max
[N-m/s], maximum wheel power
-
double linearFrictionRatio
[%] ratio relative to max speed value up to which the friction behaves linearly
-
double rWB_B[3]