Criteria for Trajectory and Exterior Orientation
The position and attitude accuracy specifications of various Leica Geosystems airborne sensors with integrated GNSS/IMU system are specified in terms of the Root Mean Square Error (RMSE) of the post-processed trajectory values. RMSE values give a robust indication of the trajectory quality with the assumptions listed below. Average and maximum limits are easily dominated with short term events that would invalidate a complete trajectory if used as pass/fail quality criteria, but do not give a clear indication of the general trajectory quality.
The recommended values are typical values. If any of the recommended values are exceeded in the processed solution, the processed solution must be reviewed in detail. The reasons for the higher values must be isolated and analyzed first by the user. Leica Geosystems Support can also review the processed solution if necessary. Often reprocessing of the recorded data with changed processing parameters or data from a different base station will improve the solution so that the values are subsequently better than the recommended values.
The following section outlines the acceptance criteria for a trajectory suitable for misalignment calculation. While the quality of the trajectory for project work can be slightly more relaxed, it should generally adhere as closely as possible to the following values or better:
Minimum requirements for acceptable differential processed tightly coupled solution
The recommendations below are based on a proper and correctly processed differential tightly coupled solution. The processed differential tightly coupled solution must have the following minimum characteristics to qualify as an acceptable solution:
Base station data used for processing must:
start before the start of the sensor data airborne recording
end after the end of the sensor data airborne recording
have a minimum data logging frequency of 1 Hz
if a GPS base station is deployed by the customer (manly in remote areas for the duration of Project) the base station should be record data for more then 2h to be able to process a proper position in post processing.
Base station position, coordinate refence system and datum must be known, correct and used in processing
Solar activity and other atmospheric conditions are minimal and acceptable
No GNSS outages or poor data
Acceptable GNSS constellation factors (acceptable average PDOP values of <2.5, during the recording, optimal is close to 1.0)
Maximum aircraft bank angle is less than 25° during the recording
Proper and suitable start and end alignment segments were recorded
No other external factors that would create erroneous or poor solution
Leverarms are measured and applied correctly
Measurement | Tolerance for entire misalignment-flight | Note |
Forward/Reverse Combined Separation | East and North< +/-3cm | Typical East/North <+/-2cm |
Forward/Reverse Attitude Separation | Roll & Pitch < +/-0.02arcmin | Typical Roll &Pitch <+/-0.01arcmin |
IMU to GNSS Misclosure | XY < 0.02m | Check Lever arm values |
Lever Arm Estimation | XYZ < 5 cm difference to measured | Check measured value |
PPP Estimation of Base station position | XY < +/-0.07m | Check Datum and Epoch |
If a trajectory exhibits lower quality than described, a misalignment calculation should not be performed without first reducing the QA criteria. The focus should be on further improving the resulting quality of the trajectory.