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                                     1.2.4 Computation of structural reliability

               An important class of limit states are those for which all the variables are treated as time
               independent, either by neglecting time variations in cases where this is considered acceptable
               or by transforming time dependent processes into time invariant variables (e.g. by using
               extreme value distributions). For these problems so-called asymptotic or simulation methods
               may be used, described in a number of reliability textbooks (e.g. Ang and Tang, 1984;
               Ditlevsen and Madsen, 1996; Madsen et al., 1986; Melchers, 1999; Thoft-Christensen and
               Baker, 1982).

               Asymptotic approximate methods
               Although these methods first emerged with basic random variables described through
               ‘second-moment’ information (i.e. with their mean value and standard deviation, but without
               assigning any probability distributions), it is nowadays possible in many cases to have a full
               description of the random vector X (as a result of data collection and probabilistic modelling
               studies). In such cases, the probability of failure could be calculated via first or second order
               reliability methods (FORM and SORM respectively). Their implementation relies on:


               (1) Transformation techniques



                                                                                                   (1.11)


               where U , U ,…, U are independent standard normal variables (i.e. with zero mean value and
                       1
                           2
                                  n
               unit standard deviation). Hence, the basic variable space (including the limit state function) is
               transformed into a standard normal space, see Figures 1.2(a) and 1.2(b). The special
               properties of the standard normal space lead to several important results, as discussed below.

               (2) Search techniques
               In standard normal space, see Figure 1.2(b), the objective is to determine a suitable checking
               point: this is shown to be the point on the limit—state surface which is closest to the origin,
               the so-called ‘design point’. In this rotationally symmetric space, it is the most likely failure
               point, in other words its co-ordinates define the combination of variables that are most likely
               to cause failure. This is because the joint standard normal density function, whose bell-shaped
               peak lies directly above the origin, decreases exponentially as the distance from the origin
               increases. To determine this point, a search procedure is generally required.
                 Denoting the co-ordinates of this point by
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