OrbitParams defines the orbital parameters of a given orbit. More...
#include <style.hpp>
Public Attributes | |
| Vec3 | initialCondition |
| The initial position of the satellite with respect to Earth (at t = 0 and theta = 0) | |
| Vec3(* | position )(int theta) |
| The position of the satellite as a function of the number of revolutions it has done. | |
| Vec3(* | majorAxis )(int theta) |
| The major axis vector as a function with respect to the revolutions of the satellite. | |
| Vec3(* | minorAxis )(int theta) |
| The minor axis vector as a function with respect to the revolutions of the satellite. | |
| decimal(* | inPlaneRotation )(int theta) |
| The angular speed that the satellite's orbit plane rotates in plane at with respect to the number of revolutions in the satellite's orbit. | |
| decimal(* | outPlaneRotation )(int theta) |
| The angular speed that the satellite's orbit plane rotates out of plane at with respect to the number of revolutions in the satellite's orbit. | |
Detailed Description
OrbitParams defines the orbital parameters of a given orbit.
Member Data Documentation
◆ inPlaneRotation
| decimal(* found::OrbitParams::inPlaneRotation) (int theta) |
The angular speed that the satellite's orbit plane rotates in plane at with respect to the number of revolutions in the satellite's orbit.
This is the same as the speed at which the major axis rotates around the barycenter of orbit in the plane of orbit, which is approximately at Earth's center
- Parameters
-
theta The number of revolutions the satellite has done
- Returns
- The angular speed at which the plane of orbit rotates at, in plane, after theta revolutions
◆ majorAxis
| Vec3(* found::OrbitParams::majorAxis) (int theta) |
The major axis vector as a function with respect to the revolutions of the satellite.
- Parameters
-
theta The number of revolutions the satellite has done
- Returns
- The major axis vector after theta revolutions have taken place
◆ minorAxis
| Vec3(* found::OrbitParams::minorAxis) (int theta) |
The minor axis vector as a function with respect to the revolutions of the satellite.
- Parameters
-
theta The number of revolutions the satellite has done
- Returns
- The minor axis vector after theta revolutions have taken place
◆ outPlaneRotation
| decimal(* found::OrbitParams::outPlaneRotation) (int theta) |
The angular speed that the satellite's orbit plane rotates out of plane at with respect to the number of revolutions in the satellite's orbit.
This is the same as the angular speed at which the plane of orbit changes
- Parameters
-
theta The number of revolutions the satellite has done
- Returns
- The angular speed at which the orbital plane rotates at, out of plane, after theta revolutions
◆ position
| Vec3(* found::OrbitParams::position) (int theta) |
The position of the satellite as a function of the number of revolutions it has done.
- Parameters
-
theta The number of revolutions the satellite has done
- Returns
- The position vector after theta revolutions have taken place
The documentation for this struct was generated from the following file:
- src/common/style.hpp
