TY - GEN
T1 - Slant range analysis and compensation of radar altimeter flight test data
AU - Spiegel, Philip
AU - Kriegel, Michael
AU - Dambeck, Johann
AU - Holzapfel, Florian
PY - 2015
Y1 - 2015
N2 - This paper introduces a high detailed radar altimeter simulation model, considering geometric and signal processing aspects. On the one hand, the simulation model is deployed in a simulation environment for a better understanding of the different error sources of radar altimeters, on the other hand, it is used inflight to compensate those errors. To evaluate the radar simulation model, the results are compared to recorded altimeter flight test data to show the strengths and weaknesses of the simulation model and the following applicability. Afterwards, the inflight use of a radar altimeter simulation model is introduced in a compensation algorithm, using the real flight test data to improve the height measurement compared to a classical radar height processing. The aiding of a compensated radar height measurement in an integrated navigation system is introduced. Finally, the performance of the algorithm is shown on an approach trajectory of a small aircraft on an airfield in hilly environment.
AB - This paper introduces a high detailed radar altimeter simulation model, considering geometric and signal processing aspects. On the one hand, the simulation model is deployed in a simulation environment for a better understanding of the different error sources of radar altimeters, on the other hand, it is used inflight to compensate those errors. To evaluate the radar simulation model, the results are compared to recorded altimeter flight test data to show the strengths and weaknesses of the simulation model and the following applicability. Afterwards, the inflight use of a radar altimeter simulation model is introduced in a compensation algorithm, using the real flight test data to improve the height measurement compared to a classical radar height processing. The aiding of a compensated radar height measurement in an integrated navigation system is introduced. Finally, the performance of the algorithm is shown on an approach trajectory of a small aircraft on an airfield in hilly environment.
UR - http://www.scopus.com/inward/record.url?scp=84938770075&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:84938770075
T3 - Institute of Navigation International Technical Meeting 2015, ITM 2015
SP - 223
EP - 233
BT - Institute of Navigation International Technical Meeting 2015, ITM 2015
PB - Institute of Navigation
T2 - Institute of Navigation International Technical Meeting 2015, ITM 2015
Y2 - 26 January 2015 through 28 January 2015
ER -