2015
DOI: 10.1049/iet-rsn.2014.0258
|View full text |Cite
|
Sign up to set email alerts
|

Interference suppression with flat gain constraint for satellite navigation systems

Abstract: Power minimisation approach is an effective interference suppression algorithm for satellite navigation systems. It forms automatically deep nulls in the direction-of-arrival (DOA) of interferences without prior information about the DOAs of satellite signals and interferences. However, it cannot provide flat gains for other directions. Thus, the desired satellite signals may be partly suppressed when they locate in the shallow nulls. By combining eigenvalue thresholding method and l1-norm constraint, a new in… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1

Citation Types

0
5
0

Year Published

2017
2017
2021
2021

Publication Types

Select...
5
4

Relationship

0
9

Authors

Journals

citations
Cited by 9 publications
(5 citation statements)
references
References 12 publications
0
5
0
Order By: Relevance
“…In this section, several simulations are constructed to evaluate the performance of the proposed method. Meanwhile, the proposed algorithm is compared with MVDR algorithm [19], PI algorothm [21], CS-SF algorithm [20], and OMP-ISRP algorithm [22]. Assume that the ULA is composed of 8 antennas with equally spaced d = 0.098m.…”
Section: Simulation Resultsmentioning
confidence: 99%
“…In this section, several simulations are constructed to evaluate the performance of the proposed method. Meanwhile, the proposed algorithm is compared with MVDR algorithm [19], PI algorothm [21], CS-SF algorithm [20], and OMP-ISRP algorithm [22]. Assume that the ULA is composed of 8 antennas with equally spaced d = 0.098m.…”
Section: Simulation Resultsmentioning
confidence: 99%
“…Consider a uniform linear antenna array of omnidirectional array elements employed in GNSS receiver, one satellite signal, and uncorrelated interference which impinge on the array at the th snapshot as expressed by [21] x…”
Section: Satellite Navigation Signal Reception Modelmentioning
confidence: 99%
“…Using the formulation from (20) and (21), the resulting update equation of weight deviation vector can be computed as…”
mentioning
confidence: 99%
“…If the gains of the non-jamming direction remain unchanged, the above problems of Adaptive Nulling would be avoided. Wenyi Wang put forward a proposal that the gains in all directions should be close to 0 dB [ 9 ].…”
Section: Introductionmentioning
confidence: 99%