DocumentCode :
2898353
Title :
The derivation of path following error and control motion noise filters for the reduction of Global Positioning System flight test data
Author :
Nelson, Andrew
Author_Institution :
Booz-Allen & Hamilton, Inc., New York, NY, USA
fYear :
1992
fDate :
23-27 Mar 1992
Firstpage :
362
Lastpage :
366
Abstract :
In order to perform a complete comparison with existing systems and properly define and analyze the error properties of the GPS (Global Positioning System), PFE (path following error), and CMN (control motion noise) filters need to be defined for use during testing activities. The author discusses PFE and CMN characteristics and how these error components affect flight and aircraft systems, and then derives digital filters that can be used to reduce GPS data into components of PFE and CMN based on international specifications
Keywords :
aerospace testing; digital filters; error analysis; radionavigation; satellite relay systems; GPS; Global Positioning System; aircraft systems; control motion noise filters; digital filters; flight systems; flight test data; international specifications; path following error; Control systems; Error analysis; Error correction; Filters; Global Positioning System; Motion analysis; Motion control; Performance analysis; Performance evaluation; System testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Position Location and Navigation Symposium, 1992. Record. 500 Years After Columbus - Navigation Challenges of Tomorrow. IEEE PLANS '92., IEEE
Conference_Location :
Monterey, CA
Print_ISBN :
0-7803-0468-3
Type :
conf
DOI :
10.1109/PLANS.1992.185868
Filename :
185868
Link To Document :
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