Unverified Commit de195ded authored by Austin Sanders's avatar Austin Sanders Committed by GitHub
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Added inline descriptions of sensor parameters (#481)

* Added inline descriptions of sensor parameters

* Added inline descriptions of sensor parameters

* Updated wording on inline comments
parent 805cea42
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+16 −16
Original line number Diff line number Diff line
@@ -49,22 +49,22 @@ const std::string UsgsAstroLsSensorModel::_SENSOR_MODEL_NAME =
    "USGS_ASTRO_LINE_SCANNER_SENSOR_MODEL";
const int UsgsAstroLsSensorModel::NUM_PARAMETERS = 16;
const std::string UsgsAstroLsSensorModel::PARAMETER_NAME[] = {
    "IT Pos. Bias   ",  // 0
    "CT Pos. Bias   ",  // 1
    "Rad Pos. Bias  ",  // 2
    "IT Vel. Bias   ",  // 3
    "CT Vel. Bias   ",  // 4
    "Rad Vel. Bias  ",  // 5
    "Omega Bias     ",  // 6
    "Phi Bias       ",  // 7
    "Kappa Bias     ",  // 8
    "Omega Rate     ",  // 9
    "Phi Rate       ",  // 10
    "Kappa Rate     ",  // 11
    "Omega Accl     ",  // 12
    "Phi Accl       ",  // 13
    "Kappa Accl     ",  // 14
    "Focal Bias     "   // 15
    "IT Pos. Bias   ",  //  0 - "In Track Position Bias" - a constant shift in the spacecraft's position parallel to the flight path 
    "CT Pos. Bias   ",  //  1 - "Cross Track Position Bias" - a constant shift in the spacecraft's position perpendicular to the flight path
    "Rad Pos. Bias  ",  //  2 - "Radial Position Bias" - a constant shift in the spacecraft's "vertical positioning," i.e. distance from the target
    "IT Vel. Bias   ",  //  3 - "In Track Velocity Bias" - a time-dependent linear shift in the spacecraft's position parallel to the flight path
    "CT Vel. Bias   ",  //  4 - "Cross Track Velocity Bias" - a time-dependent linear shift in the spacecraft's position perpendicular to the flight path
    "Rad Vel. Bias  ",  //  5 - "Radial Velocity Bias" - a time-dependent linear shift in the spacecraft's "vertical positioning," i.e. distance from the target
    "Omega Bias     ",  //  6 - The initial omega angle (analogous to "roll")
    "Phi Bias       ",  //  7 - The initial phi angle (analogous to "pitch")
    "Kappa Bias     ",  //  8 - The initial kappa angle (analogous to "yaw")
    "Omega Rate     ",  //  9 - An angular rate that allows the omega angle to vary linearly with time
    "Phi Rate       ",  // 10 - An angular rate that allows the phi angle to vary linearly with time
    "Kappa Rate     ",  // 11 - An angular rate that allows the kappa angle to vary linearly with time
    "Omega Accl     ",  // 12 - An angular acceleration that allows the omega angle to vary quadratically with respect to time
    "Phi Accl       ",  // 13 - An angular acceleration that allows the phi angle to vary quadratically with respect to time
    "Kappa Accl     ",  // 14 - An angular acceleration that allows the kappa angle to vary quadratically with respect to time
    "Focal Bias     "   // 15 - Estimated error of the camera's focal length
};

const std::string UsgsAstroLsSensorModel::_STATE_KEYWORD[] = {
+16 −16
Original line number Diff line number Diff line
@@ -48,22 +48,22 @@ const std::string UsgsAstroPushFrameSensorModel::_SENSOR_MODEL_NAME =
    "USGS_ASTRO_PUSH_FRAME_SENSOR_MODEL";
const int UsgsAstroPushFrameSensorModel::NUM_PARAMETERS = 16;
const std::string UsgsAstroPushFrameSensorModel::PARAMETER_NAME[] = {
    "IT Pos. Bias   ",  // 0
    "CT Pos. Bias   ",  // 1
    "Rad Pos. Bias  ",  // 2
    "IT Vel. Bias   ",  // 3
    "CT Vel. Bias   ",  // 4
    "Rad Vel. Bias  ",  // 5
    "Omega Bias     ",  // 6
    "Phi Bias       ",  // 7
    "Kappa Bias     ",  // 8
    "Omega Rate     ",  // 9
    "Phi Rate       ",  // 10
    "Kappa Rate     ",  // 11
    "Omega Accl     ",  // 12
    "Phi Accl       ",  // 13
    "Kappa Accl     ",  // 14
    "Focal Bias     "   // 15
    "IT Pos. Bias   ",  // 0 - "In Track Position Bias" - a constant shift in the spacecraft's position parallel to the flight path 
    "CT Pos. Bias   ",  // 1 - "Cross Track Position Bias" - a constant shift in the spacecraft's position perpendicular to the flight path
    "Rad Pos. Bias  ",  // 2 - "Radial Position Bias" - a constant shift in the spacecraft's "vertical positioning," i.e. distance from the target
    "IT Vel. Bias   ",  // 3 - "In Track Velocity Bias" - a time-dependent linear shift in the spacecraft's position parallel to the flight path
    "CT Vel. Bias   ",  // 4 - "Cross Track Velocity Bias" - a time-dependent linear shift in the spacecraft's position perpendicular to the flight path
    "Rad Vel. Bias  ",  // 5 - "Radial Velocity Bias" - a time-dependent linear shift in the spacecraft's "vertical positioning," i.e. distance from the target
    "Omega Bias     ",  // 6 - The initial omega angle (analogous to "roll")
    "Phi Bias       ",  // 7 - The initial phi angle (analogous to "pitch")
    "Kappa Bias     ",  // 8 - The initial kappa angle (analogous to "yaw")
    "Omega Rate     ",  // 9 - An angular rate that allows the omega angle to vary linearly with time
    "Phi Rate       ",  // 10 - An angular rate that allows the phi angle to vary linearly with time
    "Kappa Rate     ",  // 11 - An angular rate that allows the kappa angle to vary linearly with time
    "Omega Accl     ",  // 12 - An angular acceleration that allows the omega angle to vary quadratically with respect to time
    "Phi Accl       ",  // 13 - An angular acceleration that allows the phi angle to vary quadratically with respect to time
    "Kappa Accl     ",  // 14 - An angular acceleration that allows the kappa angle to vary quadratically with respect to time
    "Focal Bias     "   // 15 - Estimated error of the camera's focal length
};

const std::string UsgsAstroPushFrameSensorModel::_STATE_KEYWORD[] = {