Global Positioning System Reference
In-Depth Information
where b u is the user clock bias error expressed in distance, which is related to the
quantity b ut by b u
cb ut . In Equation (2.5), four equations are needed to solve
for four unknowns x u , y u , z u ,and b u . Thus, in a GPS receiver, a minimum of
four satellites is required to solve for the user position. The actual measurement
of the pseudorange will be discussed in Chapter 9.
=
2.6 SOLUTION OF USER POSITION FROM PSEUDORANGES
One common way to solve Equation (2.5) is to linearize them. The above
equations can be written in a simplified form as
(x i
ρ i =
x u ) 2
+
(y i
y u ) 2
+
(z i
z u ) 2
+
b u
( 2 . 6 )
where i = 1, 2, 3, and 4, and x u , y u , z u ,and b u are the unknowns. The
pseudorange ρ i and the positions of the satellites x i , y i , z i are known.
Differentiate this equation, and the result is
(x i
x u )δx u +
(y i
y u )δy u +
(z i
z u )δz u
δρ i =
(x i x u ) 2
+ δb u
+ (y i y u ) 2
+ (z i z u ) 2
(x i
x u )δx u
+
(y i
y u )δy u
+
(z i
z u )δz u
=
+
δb u
(2.7)
ρ i
b u
In this equation, δx u , δy u , δz u ,and δb u can be considered as the only unknowns.
The quantities x u , y u , z u ,and b u are treated as known values because one can
assume some initial values for these quantities. From these initial values a new
set of δx u , δy u , δz u ,and δb u can be calculated. These values are used to modify
the original x u , y u , z u ,and b u to find another new set of solutions. This new set
of x u , y u , z u ,and b u can be considered again as known quantities. This process
continues until the absolute values of δx u , δy u , δz u ,and δb u are very small and
within a certain predetermined limit. The final values of x u , y u , z u ,and b u are
the desired solution. This method is often referred to as the iteration method.
With δx u , δy u , δz u ,and δb u as unknowns, the above equation becomes a set of
linear equations. This procedure is often referred to as linearization. The above
equation can be written in matrix form as
δρ 1
δρ 2
δρ 3
δρ 4
α 11
α 12
α 13
1
δx u
δy u
δz u
δb u
=
α 21
α 22
α 23
1
( 2 . 8 )
α 31
α 32
α 33
1
α 41
α 42
α 43
1
where
x i x u
ρ i
y i y u
ρ i
z i z u
ρ i
α i 1 =
α i 2 =
α i 3 =
( 2 . 9 )
b u
b u
b u
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