Ginan
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ORBEX entry to write out. More...
ORBEX entry to write out.
Data Fields | |
SatSys | Sat = {} |
Satellite ID. | |
Vector3d | pos = Vector3d::Zero() |
Satellite position (m) | |
Vector3d | vel = Vector3d::Zero() |
Satellite velocity (m/s) | |
double | clk = NO_CLK |
Satellite clock (microsecond) & clock-rate (nanosecond/s) | |
double | clkVel = NO_CLK |
Vector3d | posStd = Vector3d::Ones() * NO_PV_STD |
Satellite position std (mm) | |
Vector3d | velStd = Vector3d::Ones() * NO_PV_STD |
Satellite velocity std (micrometer/s) | |
double | clkStd = NO_CLK_STD |
Satellite clock (picosecond) | |
double | clkVelStd = NO_CLK_STD |
Satellite clock-rate std (femtosecond/s) | |
Quaterniond | q = {0, 0, 0, 0} |
Satellite attitude in quaternions. | |
double OrbexEntry::clk = NO_CLK |
Satellite clock (microsecond) & clock-rate (nanosecond/s)
double OrbexEntry::clkStd = NO_CLK_STD |
Satellite clock (picosecond)
double OrbexEntry::clkVel = NO_CLK |
double OrbexEntry::clkVelStd = NO_CLK_STD |
Satellite clock-rate std (femtosecond/s)
Vector3d OrbexEntry::pos = Vector3d::Zero() |
Satellite position (m)
Vector3d OrbexEntry::posStd = Vector3d::Ones() * NO_PV_STD |
Satellite position std (mm)
Quaterniond OrbexEntry::q = {0, 0, 0, 0} |
Satellite attitude in quaternions.
SatSys OrbexEntry::Sat = {} |
Satellite ID.
Vector3d OrbexEntry::vel = Vector3d::Zero() |
Satellite velocity (m/s)
Vector3d OrbexEntry::velStd = Vector3d::Ones() * NO_PV_STD |
Satellite velocity std (micrometer/s)