Title : 
Detecting transients of unknown length
         
        
            Author : 
Wang, Z. Jane ; Willett, Peter
         
        
            Author_Institution : 
Dept. of Electr. & Comput. Eng., British Columbia Univ., Vancouver, BC
         
        
        
        
        
        
            Abstract : 
For detection of a permanent and precisely-modeled change in distribution of iid (independent and identically distributed) observations, Page\´s test is optimal. When employed to detect a transient change in distribution, Page\´s test is easy to implement and, since it is a GLRT, it provides reliable performance. However, its application to unknown transient changes is less clear. The situation of interest in this manuscript is of a transient signal of unknown scale parameter: a fixed Page procedure tuned to a "short-and-loud" signal uses heavy biasing and low threshold, a combination ill-suited to a "long-but-quiet" signal. In this paper we offer an easy adaptive alternative to the standard Page: a Page test can be thought of as a repeated sequential test, and here we propose that each of this use a time-varying threshold - specifically one that increases. The idea is that the above short signals are detected quickly before post-termination data has a chance to refute them; and that evidence for a long signal is allowed to build, rather than being summarily discarded too early. The approach works remarkably well: its performance essentially traces the "envelope" of fixed/tuned Page tests
         
        
            Keywords : 
signal detection; statistical testing; transients; Page test; long-but-quiet signal; short-and-loud signal; transients detection; unknown transient changes; Aerospace testing; Bayesian methods; Delay; Maximum likelihood detection; Sequential analysis; Signal generators; Statistical analysis; Statistics; Zinc;
         
        
        
        
            Conference_Titel : 
Aerospace Conference, 2005 IEEE
         
        
            Conference_Location : 
Big Sky, MT
         
        
            Print_ISBN : 
0-7803-8870-4
         
        
        
            DOI : 
10.1109/AERO.2005.1559517