GPS arrival angle selecting system and method
View Patent ↗Disclosed is a GPS arrival angle selecting system. The system includes: a arrival angle estimating unit connected to a receiving antenna of a GPS receiver including at least one antenna array element and configured to decide a first arrival angle of a signal received prior to despreading and a second arrival angle of a signal received after despreading; and an arrival angle selecting unit configured to select a different peak value by comparing the first arrival angle and the second arrival angle. Also disclosed is a GPS arrival angle selecting method.
1. A GPS arrival angle selecting system, comprising:
an arrival angle estimating unit connected to a receiving antenna of a GPS receiver including at least one antenna array element and configured to determine a first arrival angle of a first signal received prior to despreading and a second arrival angle of a second signal received after despreading; and
an arrival angle selecting unit configured to select a different peak value by comparing the first arrival angle and the second arrival angle to determine the GPS arrival angle wherein a beam is formed in the GPS arrival angle direction, wherein the arrival angle estimating unit includes:
a first arrival angle estimating unit connected to the receiving antenna and configured to determine a first arrival angle of peak signals by analyzing the first signal received prior to despreading through the use of an auto-correlation matrix;
a despreading unit connected to the receiving antenna and configured to increase the electric power of a GPS signal to an interference power level or more; and
a second arrival angle estimating unit configured to determine a second arrival angle of peak signals by analyzing the second signal outputted from the despreading unit through the use of an auto-correlation matrix.
2. The system of claim 1 , wherein the first arrival angle estimating unit includes:
a first matrix analyzing unit connected to the receiving antenna and configured to determine an eigenstructure of an auto-correlation matrix with respect to the first signal received prior to despreading; and
a first peak signal detecting unit configured to detect the first arrival angle of the peak signals based on the auto-correlation matrix determined by the first matrix analyzing unit.
3. The system of claim 2 , wherein the eigenstructure of the auto-correlation matrix is determined by
R x Γ=ΓΛ,
where Rx denotes the auto-correlation matrix, Λ denotes a diagonal matrix represented by Λ=diag{λ 2 , . . . , λ M } in which {λ1} is an eigenvalue, and Γ denotes a eigenvector matrix,
wherein the auto-correlation matrix is defined by
R x =E [ x ( k ) x H ( k )],
and
wherein a function for estimating the first arrival angle of the signal received prior to despreading is calculated by
P
M
(
θ
,
ϕ
)
=
1
a
H
(
θ
,
ϕ
)
Γ
M
-
L
Γ
M
-
L
H
a
(
θ
,
ϕ
)
,
where Γ M−L denotes an Mx(M−L) matrix composed of columns including M−L eigenvectors equivalent to M−L smallest eigenvalues.
4. The system of claim 2 , wherein the despreading unit is configured to generate an output based on a PRN code (C i ) of an ith satellite composed of an identical C/A code, the output of the despreading unit calculated by
x ( n )= a c Nb ( n )+ As ( n )+ v ( n ),
where b(n)) denotes a GPS data bit, s(n) is represented by s(n)=S(n)c i in which S(n) is given by S(n)=[s(k), . . . , s(k+N−1)], and v(n) is represented by v(n)=V(n)c i in which V(n) is given by V(n)=[v(k), . . . , v(k+N−1)].
5. The system of claim 4 , wherein the second arrival angle estimating unit includes:
a second matrix analyzing unit configured to determine an eigenstructure of an auto-correlation matrix with respect to the output of the despreading unit; and
a second peak signal detecting unit configured to detect the second arrival angle of the peak signals based on the auto-correlation matrix determined by the second matrix analyzing unit.
6. The system of claim 1 , further comprising:
an adaptive-array-based beam forming unit connected to the arrival angle selecting unit and configured to remove an interference signal of a selected arrival angle and to process a GPS reception signal.
7. A GPS arrival angle selecting method, comprising the steps of:
(a) if a GPS receiver including at least one antenna array element receives GPS signals, determining a first arrival angle of peak signals among the GPS signals received prior to despreading through the use of a first arrival angle estimating unit;
(b) determining a second arrival angle of peak signals among the GPS signals received after despreading through the use of a despreading unit and a second arrival angle estimating unit; and
(c) selecting a different peak value among estimated peak values through the use of an arrival angle selecting unit by comparing the first arrival angle and the second arrival angle to determine the GPS arrival angle wherein a beam is formed in the GPS arrival angle direction.
8. The method of claim 7 , wherein the step (a) includes the steps of:
(a-1) determining an eigenstructure of an auto-correlation matrix with respect to the GPS signals received prior to despreading through the use of a first matrix analyzing unit; and
(a-2) detecting the first arrival angle of the peak signals based on the auto-correlation matrix determined in the step (a-1) through the use of a first peak signal detecting unit.
9. The method of claim 8 , wherein the step (b) includes the step of:
(b-1) outputting a signal based on a PRN code (C i ) of an ith satellite composed of an identical C/A code.
10. The method of claim 9 , wherein the step (b) further includes the steps of:
(b-2) determining an eigenstructure of an auto-correlation matrix with respect to the signal outputted in the step (b-1) through the use of a second matrix analyzing unit; and
(b-3) detecting the second arrival angle of the peak signals based on the auto-correlation matrix determined in the step (c-1) through the use of a second peak signal detecting unit.