本文整理汇总了C++中SolarSystem::addCelestialBody方法的典型用法代码示例。如果您正苦于以下问题：C++ SolarSystem::addCelestialBody方法的具体用法？C++ SolarSystem::addCelestialBody怎么用？C++ SolarSystem::addCelestialBody使用的例子？那么, 这里精选的方法代码示例或许可以为您提供帮助。您也可以进一步了解该方法所在类SolarSystem的用法示例。
在下文中一共展示了SolarSystem::addCelestialBody方法的1个代码示例，这些例子默认根据受欢迎程度排序。您可以为喜欢或者感觉有用的代码点赞，您的评价将有助于系统推荐出更棒的C++代码示例。
示例1: main
int main()
{
// SET METHOD: 0 for Verlet and 1 for Runge-Kutta
int method = 1;
// SET SUN MOVEMENT ABILITY: 0 for moving sun, 1 for stationary sun
int stationarySun = 1;
// Set endpoint of time calculations and timestep (dt)
float number_of_years = 20;
double timestep = 1e-2;
// Setting initial solar system and celestial bodies
const double pi = 4*std::atan(1.0); // Pi with double-precision
const double G = 4*pi*pi;
// CelestialBody name(x, y,vx, vy, mass, radius, name);
CelestialBody sun (0, 0, 0, 0, 1, 4.64e-3, "Sun");
// CelestialBody mercury(0.39, 0, 0, 2*pi/sqrt(0.39), 1.65e-7, 1.63e-5, "Mercury");
// CelestialBody venus (0.72, 0, 0, 2*pi/sqrt(0.72), 2.45e-6, 4.03e-5, "Venus");
CelestialBody earth (1, 0, 0, 2*pi, 3e-6, 4.25e-5, "Earth");
// CelestialBody mars (1.52, 0, 0, 2*pi/sqrt(1.52), 3.2e-7, 2.26e-5, "Mars");
// CelestialBody jupiter(5.2, 0, 0, 2*pi/sqrt(5.2), 9.5e-4, 4.66e-4, "Jupiter");
// CelestialBody saturn (9.54, 0, 0, 2*pi/sqrt(9.54), 2.85e-4, 3.88e-4, "Saturn");
// CelestialBody uranus (19.19, 0, 0, 2*pi/sqrt(19.19), 4.35e-5, 1.69e-4, "Uranus");
// CelestialBody neptune(30.07, 0, 0, 2*pi/sqrt(30.07), 5.1e-5, 1.64e-4, "Neptune");
// CelestialBody pluto (39.48, 0, 0, 2*pi/sqrt(39.48), 6.55e-9, 7.67e-6, "Pluto");
SolarSystem solSyst;
solSyst.addCelestialBody(sun);
// solSyst.addCelestialBody(mercury);
// solSyst.addCelestialBody(venus);
solSyst.addCelestialBody(earth);
// solSyst.addCelestialBody(mars);
// solSyst.addCelestialBody(jupiter);
// solSyst.addCelestialBody(saturn);
// solSyst.addCelestialBody(uranus);
// solSyst.addCelestialBody(neptune);
// solSyst.addCelestialBody(pluto);
RK4 solSystRK;
int n_steps = number_of_years/timestep; // Number of calculation points
int n_bodies = solSyst.numberOfBodies();
if(method==0) // Verlet method
{
// Defining vectors for saving acceleration values
vector<double> newAcceleration = vector<double>(2*n_bodies);
vector<double> avgAcceleration = vector<double>(2*n_bodies);
// avgAcceleration must be zero at start
for(int i=0;i<2*n_bodies;i++)
{
avgAcceleration[i]=0;
}
for(int step=0;step<=n_steps;step++)
{
printf("Progress: %4.1f %% \r", 100.0*((double)step)/((double)n_steps));
solSyst.dumpToFile(timestep, step);
// Calculating forces for bodies in solar system
solSyst.calculateForces();
for (int i=stationarySun;i<n_bodies;i++)
{
CelestialBody *body = solSyst.bodies[i];
// Fetching forces acting on body
newAcceleration[2*i] = G*body->force.x()/body->mass;
newAcceleration[2*i+1] = G*body->force.y()/body->mass;
// Setting acceleration as mean value of current step and previous step
avgAcceleration[2*i] = (avgAcceleration[2*i] + newAcceleration[2*i]) /2.0;
avgAcceleration[2*i+1] = (avgAcceleration[2*i+1] + newAcceleration[2*i+1])/2.0;
// Returning acceleration to class parameter
body->acceleration.set(avgAcceleration[2*i], avgAcceleration[2*i+1], 0);
// Calculating new velocity and returning value to class parameter
double velocity_x = body->velocity.x()+ avgAcceleration[2*i] * timestep;
double velocity_y = body->velocity.y()+ avgAcceleration[2*i+1]* timestep;
body->velocity.set(velocity_x, velocity_y, 0);
// Position = previous position + v*dt + 1/2 a*dt^2, returned to calss parameter
double position_x = body->position.x()+ velocity_x * timestep + ( 0.5 * avgAcceleration[2*i] * timestep * timestep);
double position_y = body->position.y()+ velocity_y * timestep + ( 0.5 * avgAcceleration[2*i+1] * timestep * timestep);
body->position.set(position_x, position_y, 0);
}
// cout << "Sum kinetic and potential energy: " << solSyst.totalEnergy()<<endl;
// Collision test
int colltest = collisionTest(solSyst);
//.........这里部分代码省略.........