00001 #ifndef PERIAPSIS_SPACE_SATELLITE_ELEMENT_PROPAGATOR_H 00002 #define PERIAPSIS_SPACE_SATELLITE_ELEMENT_PROPAGATOR_H 00003 00004 // 00005 // $Id: satellite_element_propagator.hpp 2 2008-03-01 20:58:50Z kulibali $ 00006 // 00007 // Copyright (c) 2008, The Periapsis Project. All rights reserved. 00008 // 00009 // Redistribution and use in source and binary forms, with or without 00010 // modification, are permitted provided that the following conditions are 00011 // met: 00012 // 00013 // * Redistributions of source code must retain the above copyright notice, 00014 // this list of conditions and the following disclaimer. 00015 // 00016 // * Redistributions in binary form must reproduce the above copyright 00017 // notice, this list of conditions and the following disclaimer in the 00018 // documentation and/or other materials provided with the distribution. 00019 // 00020 // * Neither the name of the The Periapsis Project nor the names of its 00021 // contributors may be used to endorse or promote products derived from 00022 // this software without specific prior written permission. 00023 // 00024 // THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS "AS 00025 // IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT LIMITED 00026 // TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS FOR A 00027 // PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE COPYRIGHT OWNER 00028 // OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, INCIDENTAL, SPECIAL, 00029 // EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, BUT NOT LIMITED TO, 00030 // PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS OF USE, DATA, OR 00031 // PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED AND ON ANY THEORY OF 00032 // LIABILITY, WHETHER IN CONTRACT, STRICT LIABILITY, OR TORT (INCLUDING 00033 // NEGLIGENCE OR OTHERWISE) ARISING IN ANY WAY OUT OF THE USE OF THIS 00034 // SOFTWARE, EVEN IF ADVISED OF THE POSSIBILITY OF SUCH DAMAGE. 00035 // 00036 00037 #include "space/space.hpp" 00038 #include "space/propagator.hpp" 00039 00040 namespace periapsis 00041 { 00042 00043 namespace space 00044 { 00045 00046 /// Propagates using satellite elements: 00047 /// 00048 /// - a : semi-major axis (km) 00049 /// - e : eccentricity 00050 /// - w : argument of periapsis (degrees) 00051 /// - M : mean anomaly (degrees) 00052 /// - I : inclination (degrees) 00053 /// - O : longitude of the ascending node (degrees) 00054 /// - n : longitude rate (degrees/day) 00055 /// - P : sidereal period (days) 00056 /// - Pw : argument of periapsis precession period (years) 00057 /// - Pnode : longitude of ascending node precession period (years) 00058 /// - RA : right ascension of the laplace plane pole 00059 /// - DEC : declination of the laplace plane pole 00060 /// - tlit : tilt of the laplace plane 00061 /// 00062 /// Note that this transforms from kilometers/days to meters/seconds. 00063 00064 class SPACE_API satellite_element_propagator 00065 : public propagator 00066 { 00067 double data[13]; 00068 bool has_data; 00069 00070 public: 00071 satellite_element_propagator(const gsgl::data::config_record & obj_config); 00072 virtual ~satellite_element_propagator(); 00073 00074 virtual void update(const double jdn, gsgl::math::vector & position, gsgl::math::vector & velocity); 00075 00076 BROKER_DECLARE_CREATOR(periapsis::space::satellite_element_propagator); 00077 00078 private: 00079 void get_elements(const gsgl::string & str); 00080 }; // class satellite_element_propagator 00081 00082 } // namespace space 00083 00084 } // namespace periapsis 00085 00086 #endif