diff --git a/src/UsgsAstroLsSensorModel.cpp b/src/UsgsAstroLsSensorModel.cpp index 4a88aca7bc789e2ad094750085062390e606ba78..9e27bea59932323a06fa687388a7b2db3742d0c9 100644 --- a/src/UsgsAstroLsSensorModel.cpp +++ b/src/UsgsAstroLsSensorModel.cpp @@ -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[] = { diff --git a/src/UsgsAstroPushFrameSensorModel.cpp b/src/UsgsAstroPushFrameSensorModel.cpp index 10542000c09c8a554d2511ff8c050e7c0a269a33..0c933264786dc6bdc688d6a772410bc5c5a5b3b9 100644 --- a/src/UsgsAstroPushFrameSensorModel.cpp +++ b/src/UsgsAstroPushFrameSensorModel.cpp @@ -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[] = {