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Analytical Photogrammetry

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Title: Analytical Photogrammetry


1
Analytical Photogrammetry
Hande Demirel, PhD, Assistant Prof. Istanbul
Technical University (ITU), Faculty of Civil
Engineering, Geodesy and Photogrammetry
Department Division of Photogrammetry
2
Least Squares Solution
  • The method of least squares, also known as
    regression analysis, is used to model numerical
    data obtained from observations by adjusting the
    parameters of a model so as to get an optimal fit
    of the data.
  • The best fit is characterized by the sum of
    squared residuals have its least value, a
    residual being the difference between an observed
    value and the value given by the model.
  • The method was first described by Carl Friedrich
    Gauss around 1794.
  • Least squares corresponds to the maximum
    likelihood criterion if the experimental errors
    have a normal distribution.

3
Least Squares Solution
  • Gauss was able to state that the least-squares
    approach to regression analysis is optimal in the
    sense that in a linear model where the errors
    have a mean of zero, are uncorrelated, and have
    equal variances, the best linear unbiased
    estimators of the coefficients is the
    least-squares estimators. This result is known as
    the Gauss-Markov theorem.
  • In a linear model in which the errors have
    expectation zero, are uncorrelated and have equal
    variances, the best linear unbiased estimator of
    any linear combination of the observations, is
    its least-squares estimator. "Best" means that
    the least squares estimators of the parameters
    have minimum variance. The assumption of equal
    variance is valid when the errors all belong to
    the same distribution.

4
Least Squares Solution
  • The objective consists of adjusting the
    parameters of a model function so as to best fit
    a data set.
  • A simple data set consist of m points (data
    pairs) (xi, yi) , i1,m, where xi is an
    independent variable and yi is a dependent
    variable whose value is found by observation.
  • The model function has the form f(x,ß) , where
    the n adjustable parameters are held in the
    vector ß . We wish to find those parameter values
    for which the model "best" fits the data.

5
Least Squares Solution
  • The least squares method defines "best" as when
    the sum, S, of squared residuals
  • is a minimum. A residual is defined as the
    difference between the values of the dependent
    variable and the model.

6
Solving the Least Squares Problem
  • Least squares problems fall into two categories,
    linear and non-linear.
  • The linear least squares problem has a closed
    form solution, but the non-linear problem has to
    be solved by iterative refinement at each
    iteration the system is approximated by a linear
    one, so the core calculation is similar in both
    cases.

7
Least Squares Solution
For least squares solution we need linearized
observation equations
The equations (5) and (6) are nonlinear and must
be linearized.
(5)
(6)
8
Least Squares Solution
  • To linearize the equations we must expand
    them into the Taylor series and ignore the terms
    of degree 2 and higher. The differential
    quotients used in the Taylor series are as
    follows

9
Non linear Equations
xf(X0,Y0,Z0, ?,?,?, X,Y,Z)
yf(X0,Y0,Z0 ,?,?,?,X,Y,Z)
10
Non linear Equations
The Differential Quotients
.........................
.........................
11
Observation Equations
The differential quotients are used to write the
linearized observation equations of a least
squares adjustment by indirect observations.
EACH MEASURED IMAGE POINT YIELDS TWO OBSERVATION
EQUATION.
iindex for the measured point, jindex for the
photograph
12
Linearised Observation Equations
13
Linearised Observation Equations
The unknowns are the six elements (X0,Y0,Z0
,?,?,?) of outer orientation of the photograph
with the index j and the three ground
co-ordinates (X,Y,Z) of a point Pi .
The differential quotients ( )0 are calculated
from approximate values of the unknowns. For
example the approximate values of the unknowns
are put in the equation below and the value of
the differential quotient ,
is obtained.
14
Linearised Observation Equations
15
Linearised Observation Equations
and
are computed values for the functions below using
approximate values of the unknowns.
xij and yij are the measured image coordinates
16
The approximation of the Unknowns
There are various ways to derive approximations
Some of them are as follows
  • For near vertical photographs
  • ?0 ?0 0
  • ?0 is known from the flight plan
  • The co-ordinates of the projection center and the
    new points can be obtained by a block adjustment
    with independent models.

17
Example
2
1
Observed Image coordinates
1
2
3
4
3
4
2x6x448
5
6
5
6
Photo 1
Photo 2
Unknowns
3x412 Projection centre co-ordinates 3x412
Rotations 3x412 New point co-ordinates Total
36 Redundancy 48-3612
3
4
3
4
5
6
5
6
7
8
7
8
Photo 3
Photo 4
Control Point
New point
18
Observation Equations for the Example
19
Normal Equations (in matrix notation)
vAx-l (observation Equa.)
ATAxATl
ATAN and ATln
Nxn (Normal equation)
20
The Structure of Normal Equations
21
In Matrix Notation
  • N11 is a hyperdiagonal matrix with submatrices
    each of 6x6 elements
  • N22 is similary a hyperdiagonal matrix with
    submatrices of 3x3

22
In Matrix Notation
Vector of unknowns x is divided into two
subvectors x1 and x2
Subvector of the unknown outer orient. elements
Subvector of the unknown new point coordinates
23
Solution of the Normal Equations
(1)
The system can be reduced by the new point
co-ordinates x2
From the system (1) we can write
(2)
(3)
24
Solution of the Normal Equations
Multiply (3) with N22-1 from left we obtain
(4)
(5)
To eliminate x2 we replace it in Equ. (2) with
(5)
25
Solution of the Normal Equations
(The reduced equation)
26
Solution of the Normal Equations
  • An adjustment yields corrections to the
    approximate values of the elements of outer
    orientation of each photograph and to the
    approximate co-ordinates of the new points.
  • If the approximation are very poor, the corrected
    values must be treated as new approximations for
    a new adjustment.
  • This process is repeated until there is no
    further significant change in the unknowns of
    the block adjustment.

27
Accuracy of Bundle Adjustment
The accuracy can be estimated for a bundle block
adjustment with 60 overlap and 20 sidelap and
for signalised points as Planimetry sxy
3 µm in the photograph Height sz
0.03 of camera distance (NA-WA)
0.04 of camera distance
(SWA)
28
Accuracy of Bundle Adjustment
History of ?0 (Grün )
29
Advantages of Bundle Adjustment
  • Most accurate method of aerial triangulation
  • (direct relation between image and ground
    co-ordinates without of intermediate step of
    model formation)
  • Simple possibility of extending the technique to
    compensate systematic error
  • Simple possibility of incorporating external
    information in the adjustment
  • (e.g known outer orient. elements, field
    surveyed observations such as ,lengths, angles
    and geometric information)

30
Advantages of Bundle Adjustment
  • Possibility of using unconventional camera
    dispositions amateur camera photographs such as
    are often necessary in close -range
    photogrammetry.
  • Possibility of deriving the elements of outer
    orient. To be set in particular analogue or
    analytical plotters.
  • Possibility of combined adjustment with
    co-ordinates of the projection centres determined
    by kinematic GPS positioning.
  • Possibility of self calibration by additional
    parameters and determination of Systematic Image
    Error

31
Disadvantages of Bundle Adjustment
  • Nonlinear problem for which approximations can
    only be established after long procedures.
  • Computer intensive method.
  • Analogue instruments can not be used for the
    measurements.
  • Always a spatial problem,so that separate
    adjustments in planimetry and height are not
    possible.

32
Bundle Adjustment
  • To obtain a band matrix the photograph must be
    numbered vertical to the flight direction. With
    the band matris structure we can avoid the
    multiplications with zero element and spare time
    by computing
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