def apply(self, satellite: Satellite) -> ManeuverCost:
satellite.wait_time(self.delta_t)
return ManeuverCost(delta_t=self.delta_t)
ax.scatter3D(0, 0, 0) # Plot some orbits geosync = Orbit.circular_with_period(KERBIN, 21549.425 * SECS) radius = geosync.semimajor_axis sat = Satellite(KERBIN, radius * Vec3.X, geosync.speed_at(radius) * Vec3.Y) plot_orbit(sat.orbit) BoostPrograde(200 * METERS / SECS).apply(sat) plot_orbit(sat.orbit) WaitTime(sat.orbit.period / 4).apply(sat) BoostPrograde(200 * METERS / SECS).apply(sat) plot_orbit(sat.orbit) sat.wait_time(sat.orbit.period / 5) BoostPrograde(-50 * METERS / SECS).apply(sat) plot_orbit(sat.orbit) WaitApoapsis().apply(sat) PlaneChange(math.pi / 6).apply(sat) plot_orbit(sat.orbit) PlaneChange(math.pi / 3).apply(sat) plot_orbit(sat.orbit) # Plot the satellite ax.scatter3D(*sat.pos.measure(1000 * METERS)) WaitAngle(math.pi / 2).apply(sat)
