#include <MagUpdate.h>
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| clockwerk::DataIO< clockwerk::CartesianVector< 3 > > | pos_B_pI__pI = clockwerk::DataIO<clockwerk::CartesianVector<3>>(this, "pos_B_pI__pI", clockwerk::CartesianVector<3>({0.0, 0.0, 0.0})) |
| clockwerk::DataIO< clockwerk::CartesianVector< 3 > > | vel_B_pI__pI = clockwerk::DataIO<clockwerk::CartesianVector<3>>(this, "vel_B_pI__pI", clockwerk::CartesianVector<3>({0.0, 0.0, 0.0})) |
| clockwerk::DataIO< clockwerk::Quaternion > | quat_B_pI = clockwerk::DataIO<clockwerk::Quaternion>(this, "quat_B_pI", clockwerk::Quaternion({1.0, 0.0, 0.0, 0.0})) |
| clockwerk::DataIO< clockwerk::CartesianVector< 3 > > | gyroBias_B_pI__pI = clockwerk::DataIO<clockwerk::CartesianVector<3>>(this, "gyroBias_B_pI__pI", clockwerk::CartesianVector<3>({0.0, 0.0, 0.0})) |
| clockwerk::DataIO< clockwerk::CartesianVector< 3 > > | accelBias_B_pI__pI = clockwerk::DataIO<clockwerk::CartesianVector<3>>(this, "accelBias_B_pI__pI", clockwerk::CartesianVector<3>({0.0, 0.0, 0.0})) |
| clockwerk::DataIO< clockwerk::Matrix< 16, 16 > > | state_cov = clockwerk::DataIO<clockwerk::Matrix<16, 16>>(this, "state_cov", clockwerk::Matrix<16, 16> ()) |
| clockwerk::DataIO< clockwerk::Time > | state_output_time_stamp = clockwerk::DataIO<clockwerk::Time>(this, "state_output_time_stamp", clockwerk::Time(0, 0)) |
| clockwerk::DataIO< clockwerk::CartesianVector< 3 > > | pre_residual = clockwerk::DataIO<clockwerk::CartesianVector<3>>(this, "pre_residual", clockwerk::CartesianVector<3>({0.0, 0.0, 0.0})) |
| clockwerk::DataIO< clockwerk::CartesianVector< 3 > > | post_residual = clockwerk::DataIO<clockwerk::CartesianVector<3>>(this, "post_residual", clockwerk::CartesianVector<3>({0.0, 0.0, 0.0})) |
◆ Outputs()
◆ accelBias_B_pI__pI
The accelerometer bias provided as an acceleration of the body (B) frame with respect to the acceleration of the pseudo-inertial (pI) frame as provided in pseudo-inertial (pI) frame coordinates. This value is part of the inertial navigation state vector that and is post measurement incorporation. (meters/seconds^2)
◆ gyroBias_B_pI__pI
The gyrocsope bias provided as an angular velocity of the body (B) frame with repsect to the angular velocity of the pseudo-inertial (pI) frame as provided in pseudo-inertial (pI) frame coordiantes. This value is part of the inertial navigation state vector and is post measurement incorporation. (radians/second)
◆ pos_B_pI__pI
The position of the body (B) with respect to the pseudo-inertial (pI) frame as provided in pseudo-inertial (pI) frame coordinates. This value is part of the inertial navigation state vector and is post measurement incorporation. (meters)
◆ post_residual
The post update measurement residual
◆ pre_residual
The pre update measurement residual
◆ quat_B_pI
The attitude of the body (B) frame with respect to the pseudo-inertial (pI) frame as provided as a unit quaternion. This value is part of the inertial navigation state vector and is post measurement incorporation. (unitless)
◆ state_cov
The covariance matrix of the state vector. The covariances of the state random variable are defined diagonally in the order of [pos, vel, quat, gyroBias, accelBias] and are in the same units, frames, and relativistic states as the state vector definitions. This value is post measurement incorporation.
◆ state_output_time_stamp
Time stamp of the output state. The time does not need to be measured relative to anything specific as long as all time stamps are measured relative to the same epoch, e.g. mission start, J2000, MJD. (seconds)
◆ vel_B_pI__pI
The velocity of the body (B) with respect to the pseudo-inertial (pI) frame as provided in pseudo-inertial (pI) frame coordinates. This value is part of the inertial navigation state vector and is post measurement incorporation. (meters/second)
The documentation for this struct was generated from the following file:
- /Users/mickey/Documents/Projects/warptwin/warpos/src/apps/gnc/InertialNavigationEKF/MagUpdate.h