文件列表:

actuator.cpp (5682, 2003-11-27)
aerodynamics.cpp (23340, 2003-10-15)
class_functions.cpp (8971, 2013-04-26)
class_hierarchy.hpp (12479, 2008-03-19)
control.cpp (27104, 2013-10-26)
doc.asc (118395, 2013-10-26)
documentation.asc (12100, 2013-10-26)
environment.cpp (6704, 2003-09-29)
euler.cpp (3554, 2003-11-27)
execution.cpp (19899, 2013-10-26)
f16_aero_deck.asc (8371, 2003-07-24)
f16_prop_deck.asc (2135, 2003-07-24)
f16c09_7.asc (3717, 2003-10-22)
f16c09_8.asc (10308, 2003-10-15)
f16c11_1.asc (3797, 2003-10-15)
f16c11_2.asc (4280, 2003-10-15)
f16c11_3.asc (4330, 2003-10-15)
f16c11_7.asc (6307, 2003-10-09)
FALCON6.suo (72192, 2013-08-04)
forces.cpp (2522, 2003-08-05)
global_constants.hpp (1845, 2003-07-29)
global_functions.cpp (28263, 2013-10-26)
global_header.hpp (32497, 2008-03-10)
guidance.cpp (8580, 2013-04-26)
input.asc (6322, 2013-10-26)
input_copy.asc (6307, 2013-10-26)
kinematics.cpp (9892, 2003-11-27)
newton.cpp (8867, 2003-11-27)
plane_functions.cpp (42331, 2013-04-26)
propulsion.cpp (7529, 2003-11-27)
utility_functions.cpp (51221, 2013-04-26)
utility_header.hpp (10804, 2008-03-09)

/////////////////////////////////////////////////////////////////////// ////////////////////////////// FALCON6 Readme ///////////////////////// /////////////////////////////////////////////////////////////////////// ####################################################################### #### This C++ simulation is an adaptation of the FORTRAN FALCON6 #### #### 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 3.1, 25 Oct 2013 Compatible with MS C++ V12 (2013) * Release 3.0, 23 March 2013 Built with MS Visual C++ 10; compatible with MS Visual C++ 8 & 9 * Features of simulation * 6 DoF, flat Earth; local level coordinates: North, East, Down * F16 like airplane aerodynamic table deck (NASA data) single tubojet, propulsion deck autopilot: rate and acceleration guidance: line guidance, waypoint guidance * This simulation is used in it's FORTRAN version in my book * For detailed instructions and derivations of this C++ version, see my Self_Study Course "Fundamentals..." (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: * f16c09_7.asc Altitude and heading autopilot * f16c09_8.asc Altitude gain sensitivity gainalt = 0.2, 0.3, 0.4 * f16c11_1.asc Lateral and pitch acceleration * f16c11_2.asc Pitch line guidance * f16c11_3.asc Lateral line guidance * f16c11_7.asc 3 Waypoints and terminal glide slope to IP 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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