Title :
Adaptive array beamforming using a combined LMS-LMS algorithm
Author :
Srar, Jalal Abdulsayed ; Chung, Kah-Seng ; Mansour, Ali
Author_Institution :
Dept. of Electr. & Comput. Eng., Curtin Univ. of Technol., Perth, WA, Australia
Abstract :
A new adaptive algorithm, called LLMS, which employs two Least Mean Square (LMS) sections in tandem, is proposed for different applications of array beamforming. The convergence of the LLMS algorithm is analyzed, in terms of mean square error, in the presence of Additive White Gaussian Noise (AWGN) for two different operation modes; normal referencing and self-referencing. Computer simulation results show that the convergence performance of LLMS is superior to the conventional LMS algorithms as well some of the more recent LMS based algorithms, such as constrained-stability LMS (CSLMS), and Modified Robust Variable Step Size LMS (MRVSS) algorithms. It is shown that the convergence of LLMS is quite insensitive to variations in both the input signal-to-noise ratio and the step size used. Also, the operation of the proposed algorithm remains stable even when its reference signal is corrupted by AWGN noise. Furthermore, the fidelity of the signal at the output of the LLMS beamformer is demonstrated through the Error Vector Magnitude (EVM) and the scatter plot obtained.
Keywords :
AWGN; antenna arrays; array signal processing; least mean squares methods; AWGN; adaptive array beamforming; additive white Gaussian noise; combined LMS-LMS algorithm; computer simulation; constrained-stability LMS; error vector magnitude; least mean square sections; mean square error; modified robust variable step size LMS; normal referencing; self-referencing; AWGN; Adaptive algorithm; Adaptive arrays; Additive white noise; Algorithm design and analysis; Application software; Array signal processing; Convergence; Least squares approximation; Mean square error methods;
Conference_Titel :
Aerospace Conference, 2010 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
978-1-4244-3887-7
Electronic_ISBN :
1095-323X
DOI :
10.1109/AERO.2010.5446967