This paper discusses the prediction and monitoring of system integrity in the position domain. Combining two recently developed concepts for positioning performance assessment and optimization, it shows how optimized parameter estimation can be achieved. The paper shows how this optimization can be applied in a Global Navigation Satellite System (GNSS) environment for combining the measurements from multiple receivers to obtain optimally estimated differential corrections, or to combine the measurements from multiple satellites to obtain optimal integrity in the position estimate.
Integrity in the position or correction domain [satellite navigation]
2001 IEEE Aerospace Conference Proceedings (Cat. No.01TH8542) ; 3 ; 3/1293-3/1301 vol.3
2001-01-01
819201 byte
Conference paper
Electronic Resource
English
A MULTIPLE HYPOTHESIS APPROACH TO SATELLITE NAVIGATION INTEGRITY
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