GPS Failure Detection by Autonomous Means Within the Cockpit

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Volumn 33, Issue 4, 1986, Pages 335-353

  BROWN, GROVER ^a   HWANG, PATRICK Y C ^b  

^a IOWA STATE UNIVERSITY   (United States)

^b Rockwell Int Corp   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIR NAVIGATION - FAILURE; ELECTRONIC EQUIPMENT - APPLICATIONS; PROBABILITY; SIGNAL FILTERING AND PREDICTION - KALMAN FILTERING;

FAILURE DETECTION SYSTEM; GLOBAL POSITIONING SYSTEMS; KALMAN FILTER MODEL; MULTIPLE MODEL ESTIMATION ALGORITHM; NAVIGATION SYSTEM FAILURE;

SATELLITES;

EID: 0023670572     PISSN: 00281522     EISSN: 21614296     Source Type: Journal    
DOI: 10.1002/j.2161-4296.1986.tb01485.x     Document Type: Article

References (10)

1. Optimal Adaptive Estimation of Sampled Stochastic Processes
2. A New Look at the Magill Adaptive Filter as a Practical Means of Multiple Hypothesis Testing
3. A Kalman Filter Approach to Precision GPS Geodesy
4. GPS Integrity Channel