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AP_NavEKF2: Use correct casting of integers when printing

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Changes in response to review comments
This commit is contained in:
Paul Riseborough 2015-11-06 14:11:22 +11:00 committed by Andrew Tridgell
parent 987d261109
commit 65e4a4ab94
1 changed files with 5 additions and 5 deletions
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10
libraries/AP_NavEKF2/AP_NavEKF2_Control.cpp
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@ -123,7 +123,7 @@ void NavEKF2_core::setAidingMode()
stateStruct.position.z = -meaHgtAtTakeOff;
} else if (frontend->_fusionModeGPS == 3) {
// We have commenced aiding, but GPS useage has been prohibited so use optical flow only
hal.console->printf("EKF2 IMU%i is using optical flow\n",imu_index);
hal.console->printf("EKF2 IMU%u is using optical flow\n",(unsigned)imu_index);
PV_AidingMode = AID_RELATIVE; // we have optical flow data and can estimate all vehicle states
posTimeout = true;
velTimeout = true;
@ -133,7 +133,7 @@ void NavEKF2_core::setAidingMode()
prevFlowFuseTime_ms = imuSampleTime_ms;
} else {
// We have commenced aiding and GPS useage is allowed
hal.console->printf("EKF2 IMU%i is using GPS\n",imu_index);
hal.console->printf("EKF2 IMU%u is using GPS\n",(unsigned)imu_index);
PV_AidingMode = AID_ABSOLUTE; // we have GPS data and can estimate all vehicle states
posTimeout = false;
velTimeout = false;
@ -169,7 +169,7 @@ void NavEKF2_core::checkAttitudeAlignmentStatus()
tiltErrFilt = alpha*temp + (1.0f-alpha)*tiltErrFilt;
if (tiltErrFilt < 0.005f && !tiltAlignComplete) {
tiltAlignComplete = true;
hal.console->printf("EKF2 IMU%i tilt alignment complete\n",imu_index);
hal.console->printf("EKF2 IMU%u tilt alignment complete\n",(unsigned)imu_index);
}
// Once tilt has converged, align yaw using magnetic field measurements
@ -179,7 +179,7 @@ void NavEKF2_core::checkAttitudeAlignmentStatus()
stateStruct.quat = calcQuatAndFieldStates(eulerAngles.x, eulerAngles.y);
StoreQuatReset();
yawAlignComplete = true;
hal.console->printf("EKF2 IMU%i yaw alignment complete\n",imu_index);
hal.console->printf("EKF2 IMU%u yaw alignment complete\n",(unsigned)imu_index);
}
}
@ -244,7 +244,7 @@ void NavEKF2_core::setOrigin()
// define Earth rotation vector in the NED navigation frame at the origin
calcEarthRateNED(earthRateNED, _ahrs->get_home().lat);
validOrigin = true;
hal.console->printf("EKF2 IMU%i Origin Set\n",imu_index);
hal.console->printf("EKF2 IMU%u Origin Set\n",(unsigned)imu_index);
}
// Commands the EKF to not use GPS.