• DocumentCode
    3513690
  • Title

    Optimized Bernoulli Trial Technique for M Out of N Binary Integration of Radar Signals

  • Author

    Golestani, Yahya ; Mallean, George

  • Author_Institution
    Civil & Commercial Oper., Aerosp. Corp., Pasadena, CA
  • fYear
    2008
  • fDate
    1-8 March 2008
  • Firstpage
    1
  • Lastpage
    8
  • Abstract
    Binary integration is used in radar systems where M successful events out of N trials represent the detection of a target where multiple pulse-repetition frequencies (PRFs) are used. If the probabilities of the single events are equal, the probability of M events occurring out of N can be represented by a binomial distribution. If, however, switching the PRF at each event causes differing clutter to interfere with the signal, the event probabilities are not binomially distributed but are represented by a more complicated polynomial. An optimization procedure is presented that minimizes the radar resources needed for the M out of N binary integration of detector outputs with unequal signal-to-interference noise ratios (SINRs). The amount of coherent integration for each PRF output is optimally adjusted to yield a minimum total integration time over the batch of PRFs. The optimized integration time is computed for a number of different sequences of detector output SINRs and compared to the results from a binomial distribution.
  • Keywords
    binomial distribution; integration; optimisation; probability; radar signal processing; binary integration; binomial distribution; coherent integration; event probabilities; optimization procedure; optimized Bernoulli trial technique; radar signals; Clutter; Computational modeling; Detectors; Distributed computing; Event detection; Frequency; Lagrangian functions; Polynomials; Radar detection; Signal to noise ratio;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2008 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4244-1487-1
  • Electronic_ISBN
    1095-323X
  • Type

    conf

  • DOI
    10.1109/AERO.2008.4526428
  • Filename
    4526428