#include <DeadReckon.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> ()) |
◆ 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 should somewhat with the time of the incoming IMU measurement. (meters/seconds^2)
◆ gyroBias_B_pI__pI
The gyrocsope bias provided as an angular velocity of the body (B) frame with respect to the angular velocity of the pseudo-inertial (pI) frame as provided in pseudo-inertial (pI) frame coordinates. This value is part of the inertial navigation state vector and should somewhat align with the time of the incoming IMU measurement - time_in. (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 aligned with the time of output - time_in. (meters)
◆ 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 should somewhat align with the time of the incoming IMU measurement. (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.
◆ 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 should somewhat align with the time of the incoming IMU measurement. (meters/second)
The documentation for this struct was generated from the following file:
- /Users/mickey/Documents/Projects/warptwin/warpos/src/apps/gnc/InertialNavigationEKF/DeadReckon.h