private void button_caculate_Click(object sender, EventArgs e1)
{
xyzs.Clear();
double a = double.Parse(textBox_a.Text);
double e = double.Parse(this.textBox_e.Text);
double i0 = double.Parse(this.textBox_i.Text);
double M = double.Parse(this.textBox_M.Text);
double Ω = double.Parse(this.textBox_Ω.Text);
double omiga = double.Parse(this.textBox_omiga.Text);
double interval = double.Parse(textBox_interval.Text);
double epochCount = double.Parse(textBox_epochCount.Text);
CelestialMomentEllipseOrbit orbit = new CelestialMomentEllipseOrbit(omiga, i0, Ω, new MomentEllipseOrbit(M, new PlaneEllipse(a, e)));
StringBuilder sb = new StringBuilder();
for (double i = 0, t = 0; i < epochCount; i++, t += interval)
{
var xyz = KeplerOrbitUtil.GetSatPos(t, i0, Ω, a, e, omiga, M);
var op = new MomentEllipseOrbit(M, t, new PlaneEllipse(a, e));
var ceXyz = op.GetCelestialMotionState(omiga, i0, Ω);
var differXyz = xyz - ceXyz;
var three = orbit.GetMotionState(t);
var differ2 = xyz - three;
xyzs.Add(xyz);
sb.AppendLine(xyz.ToString());
}
var state = KeplerOrbitUtil.GetSatPos(0, i0, Ω, a, e, omiga, M);
var param = KeplerOrbitUtil.GetKeplerEphemerisParam(state);
var orbit2 = new CelestialMomentEllipseOrbit(state);
var tweo = orbit2.MotionState;
var state2 = KeplerOrbitUtil.GetSatPos(0, param);
var differ = state - state2;
var dirre = state - tweo;
int ii = 0;
//double dt = double.Parse(this.textBox_dt.Text);
//XYZ xyz = KeplerOrbitSolver.GetSatPos(dt, i0, Ω, Math.Sqrt(a), e, omiga, M);
//XYZ pos = XYZ.Parse(this.textBox_a.Text);
//XYZ speed = XYZ.Parse(this.textBox_dt.Text);
//Time time = Time.Parse(this.dateTimePicker1.Value);
//OrbitParamCaculator caculator = new OrbitParamCaculator();
//this.param = caculator.CaculateOrbitParam(pos, speed, time.SecondsOfWeek);
this.textBox_show.Text = sb.ToString();
this.RichTextBoxControl_processInfo.Text = "计算完毕！";
}
private void button_solveOrbitParam_Click(object sender, EventArgs e)
{
XYZ pos = XYZ.Parse(this.textBox_pos.Text);
XYZ vel = XYZ.Parse(this.textBox_vel.Text);
MotionState state = new MotionState(pos, vel);
CelestialMomentEllipseOrbit orbit = new CelestialMomentEllipseOrbit(state);
textBox_a.Text = orbit.MomentEllipseOrbit.PlaneEllipse.a + "";
this.textBox_e.Text = orbit.MomentEllipseOrbit.PlaneEllipse.e + "";
this.textBox_i.Text = orbit.Inclination + "";
this.textBox_M.Text = orbit.MomentEllipseOrbit.MeanAnomaly + "";
this.textBox_Ω.Text = orbit.RightAscensionOfAscendingNode + "";
this.textBox_omiga.Text = orbit.ArgumentOfPerigee + "";
MessageBox.Show("轨道参数已更新！");
}
