文件列表:

class_functions.cpp (13832, 2013-07-04)
class_hierarchy.hpp (19601, 2013-07-04)
cruise3_aero_deck.asc (709, 2000-10-24)
cruise3_prop_deck.asc (1523, 2001-04-22)
CRUISE5.suo (72192, 2013-08-04)
cruise_functions.cpp (43773, 2013-07-04)
cruise_modules.cpp (74301, 2007-06-08)
doc.asc (24913, 2013-10-26)
documentation.asc (15516, 2013-10-26)
execution.cpp (22564, 2013-08-04)
global_constants.hpp (1922, 2006-12-13)
global_functions.cpp (46786, 2013-08-04)
global_header.hpp (20931, 2007-03-05)
inguid1.asc (4061, 2013-08-04)
input.asc (4061, 2013-10-26)
input_copy.asc (4063, 2013-10-26)
insat2.asc (6701, 2007-06-08)
insat3.asc (9879, 2013-08-04)
round3_modules.cpp (13294, 2007-01-20)
satellite_functions.cpp (10069, 2013-07-04)
satellite_modules.cpp (1962, 2007-03-07)
target_functions.cpp (9700, 2013-07-04)
target_modules.cpp (4935, 2007-03-07)
utility_functions.cpp (54821, 2013-07-04)
utility_header.hpp (23655, 2013-07-04)

/////////////////////////////////////////////////////////////////////// ////////////////////////////// CRUISE5 Readme ///////////////////////// /////////////////////////////////////////////////////////////////////// ####################################################################### #### This C++ simulation is an adaptation of the FORTRAN CRUISE5 #### #### program, which was originally provided for my book #### #### "Modeling and Simulation of Aerospace Vehicle Dynamics". For #### #### the third Edition it was converted for the CADAC++ framework. #### #### It is 'Academic Software' and can be used and modified freely #### #### Peter Zipfel #### ####################################################################### * Release 3.0, 3 July 2013 Built with MS Visual C++ 10; compatible with MS Visual C++ 8 & 9 * Features of simulation * 3 DoF, round, rotating earth; coordinates: longitude, latitude, altitude * Cruise missile: drag polars, functions of Mach turbojet propulsion deck controllers: flight path angles, accelerations, altitude guidance: line guidance, point guidance, arc guidance, pro-nav seeker: simple line-of-sight * Targets fixed, constant speed or accelerated * Satellites orbiting the Earth, providing coordinates of (moving) targets * This simulation is used in it's FORTRAN version in my book, but has much extended capabilities, however the simple INS/GPS model is not included * For detailed instructions and derivations of this C++ version, see my Self_Study Course "Building..." (reference below) EXECUTION: * Build a project in the Visual C++ Editor with the provided source code * Execute with file 'input.asc' located in the projet directory * Plot results of output 'plot1.asc' or 'traj.asc' with KPLOT (CADAC Studio) OPTIONS: * inguid1.asc Waypoint/line guidance against GPS target coordinates * insat2.asc 1 missile vs 2 target with 2 passive satellites * insat3.ac 2 crs,2 trgt,2 sat; sats replace last waypoint, seeker terminal PLOTTING: Install KPLOT from CADAC4/Studio (free download from AIAA.org) REFERENCES: Zipfel, Peter H, "Modeling and Simulation of Aerospace Vehicle Dynamics", AIAA Education Series, 3rd Edition 2014, American Insitute of Aeronautics and Astronautics, 1801 Alexander Bell Drive, Reston, VA 20191, www.aiaa.org Zipfel, Peter H, "Building Aerospace Simulations in C++", 3rd Edition, AIAA Self-Study Series, 2nd Ed 2014 Zipfel, Peter H, "Fundamentals of 6 DoF Aerospace Simulation and Analysis in C++", AIAA Self-Study Series,2014 Zipfel, Peter H, "Advanced 6 DoF Aerospace Simulation and Analysis in C++", AIAA Self-Study Series, 2014

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