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Table 5.2 Java2WSDL Command Line Options Whenever a Java class is processed by a Java2WSDL tool, it assumes that the package namespace is the target namespace as well. Hence, in order to provide a new mapping of package name to the WSDL namespace, this argument must be provided. By default, the Java2WSDL tool would generate a WSDL document named as the package namespace, preceded by Definitions_ . Thus, in order to give a new name to the WSDL definition document, we can use this argument. This argument specifies the directory where the output WSDL definition would be stored. The default is the current directory.

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The predominant launch systems for GSO satellites have expendable boosters which employ several steps for inserting a satellite into its final orbit. The first step usually involves a few rocket firing phases which place the satellite and its attached apogee rocket motor (ARM) into a transfer orbit with a perigee of approximately 200 km in altitude and an apogee at the GSO altitude. At apogee, the ARM is fired to circularize the orbit into a geosynchronous mode. Some available launch systems with these characteristics include the ARIANE, ATLAS, DELTA, H-Series, LLV, LONG MARCH, M-Series, PROTON, TITAN, ZENIT, among others. A brief description of the capabilities of these systems is provided in the following sections. There has been interest in developing reusable launchers in which the launch vehicle is returned to Earth intact and then readied for the next launch. An example is NASA's space transportation system (Space Shuttle), which places satellites into low-Earth orbit from which an intermediate rocket inserts the satellite into a GSO transfer orbit. Then the ARM can be fired to achieve the final orbit. Since the Space Shuttle carries a human crew, its costs are too high to be practical for the many commercial communication satellites that need to be placed into orbit. It is reserved for launching special payloads or performing special operations that require human intervention. New initiatives have been reported about the development of small reusable launch vehicles (Kistler Co.) for operations in the next decade.

is the initial volatility surface, fk(m, t) are expanded eigenvectors (eigenfunctions) on the basis of a family of smooth functions (surfaces) (hj), that is, spline functions commonly used for interpolating volatility surfaces and yield curves, fi (m, ) =

Listing 3.9 Ant build script for ACME DAO classes. (continues)

If you want to convert just the expression within the parentheses to a value, get into cell edit mode and select the part that you want to evaluate. In this example, select 145*1.05. Then, press F9 followed by Enter. Excel converts the formula to the following:

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**********************************************************************************/ class G2 : public TwoFactorModel, public Af neModel, public TermStructureConsistent Model { public: G2(const RelinkableHandle<TermStructure>& termStructure, double a = 0.1, double sigma = 0.01, double b = 0.1, double eta = 0.01, double rho = 0.9); Handle<ShortRateDynamics> dynamics() const; double discountBondOption(Option::Type type, double strike, Time maturity, Time bondMaturity) const; double swaption(const Instruments::SwaptionArguments& arguments) const; DiscountFactor discount(Time t) const { return termStructure()->discount(t); } protected: void generateArguments(); double A(Time t, Time T) const; // parameter of discount bond double B(double x, Time t) const; // parameter of discount bond private: class Dynamics; // G2 dynamics class FittingParameter; // analytical term-structure tting // parameter double sigmaP(Time t, Time s) const; // bond volatility Parameter& a_; // drift of x process Parameter& sigma_; // volatility of x process Parameter& b_; // drift of y process Parameter& eta_; // volatility of y process Parameter& rho_; // correlation of Brownian motions Parameter phi_; // shift parameter double V(Time t) const; double a() const { return a_(0.0); } double sigma() const { return sigma_(0.0); } double b() const { return b_(0.0); } double eta() const { return eta_(0.0); } double rho() const { return rho_(0.0); } class SwaptionPricingFunction; friend class SwaptionPricingFunction; };

Table 9.1 describes the standard exceptions in Python. Prior to Python 1.5, all exceptions were identified as string objects; however, in Python 1.5 and later versions, most exceptions are provided as class objects. The exceptions are defined in the exceptions module. You do not need to import the exceptions module explicitly. All the exceptions are built in the namespace by default.

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