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When a developer chooses to use CMP, these control methods are provided by the WebLogic container When BMP is chosen, the developer overrides these control methods The default behavior of an entity bean, where the e jbLoad () method is called every time a read of the data store is necessary, and ejbStore () is called at every commit, might not be desirable under certain circumstances In these cases, the default behavior can be changed by manipulating some deployment descriptor elements of the bean, as we'll see next

We aim the torpedo at the target by making the initial value of phi equal to psi The initial values of u and v are set to 0 We control the rudder to keep the torpedo turned toward the target Such simple pursuit guidance works only for low target speeds unless initially one is

The behavior of the entity bean can be configured with the following tags: Q Q Q db-is-shared is-modified-method-name delay-updates-until-end-of-tx

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Policies are associated with an entity with a construct called has Below is an example policy:

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-GUIDED-TORPEDO SIMULATION -(x, y) is torpedo, (xt, yt) is target -------------------------------------------------------------------------------------------------irule 4 | ERMAX = 01 | -variable-step RK4 display N1 | display C8 | display R | scale = 2 DT = 000001 | TMAX = 2 | NN = 20000 -------------------------------------------------------------------------------------------------UC = 8 | -torpedo parameters a1 = 08155 | a2 = 08155 UT = a1 * UC^2 b1 = - 15701 | b2 = - 023229 | b3 = 0 c1 = - 303801 | c2 = - 44866 | c3 = 500 -------gain = 300 | rumax = 025 | -control parameters RR = 001 | rr = RR^2 | -distance to target DD = 100 * rr -------vxt = 01 | vyt = - 05 | -target velocity vector x=-2 | y=0 | -initial values xt0 = 1 | yt0 = 2 rudder = 0 phi = atan2(yt0 - y, xt0 - x) | -first aim at target drunr DYNAMIC -------------------------------------------------------------------------------------------------xt = xt0 + vxt * t | yt = yt0 + vyt * t | -target psi = atan2(yt - y, xt - x) | -target angle dd = (x - xt)^2 + (y - yt)^2 | -squared distance -----------------------d/dt u = UT - a2 * u^2 | -state equations d/dt v = u * (b1 * v + b2 * phidot + b3 * rudder) d/dt phidot = u * (c1 * v + c2 * phidot + c3 * rudder) d/dt phi = phidot d/dt x = u * cos(phi) - v * sin(phi) d/dt y = u * sin(phi) + v * cos(phi) -error = (phi-psi) | -control step | -this is needed for sat() rudder = - rumax * sat(gain * error) -term rr - dd | -terminate when close -------------------------------------------------------------------------------------------------DISPXY x, y, xt, yt | -draw 2 xy plots

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