This frame is an extension of the two-body rotating frame, where a scale factor is used to scale the position and velocity of the state based on the distance between the primary and secondary bodies.
| Type | Visibility | Attributes | Name | Initial | |||
|---|---|---|---|---|---|---|---|
| type(celestial_body), | public | :: | secondary_body | = | body_moon |
the secondary body used to construct the frame |
|
| integer, | public | :: | center | = | center_at_barycenter |
the frame center (can be primary_body,secondary_body, or barycenter) |
|
| real(kind=wp), | public, | dimension(6) | :: | rv12 | = | zero |
[r,v] of secondary body w.r.t. primary body |
| logical, | public | :: | inertial | = | .false. |
to make it a quasi-inertial frame (cdot is zero) |
|
| real(kind=wp), | public | :: | scale | = | zero |
scale factor |
Constructor for a two_body_rotating_pulsating_frame
| Type | Intent | Optional | Attributes | Name | ||
|---|---|---|---|---|---|---|
| type(celestial_body), | intent(in) | :: | primary_body |
the primary body of the frame |
||
| type(celestial_body), | intent(in) | :: | secondary_body |
the secondary body used to construct the frame |
||
| integer, | intent(in) | :: | center |
the frame center (can
be |
||
| real(kind=wp), | intent(in) | :: | scale |
scale factor |
||
| real(kind=wp), | intent(in) | :: | et |
epoch at which the frame is defined [sec] |
coordinate transformation routine
Transform a Cartesian state from one reference frame to another at
a specified epoch. The from and to reference_frames may each
be defined at a different epoch. The et ephemeris time is the time
the transformation is to be done, and accounts for the motion of the two
frame centers from from%et and to%et to et.
| Type | Intent | Optional | Attributes | Name | ||
|---|---|---|---|---|---|---|
| class(reference_frame), | intent(inout) | :: | from | |||
| real(kind=wp), | intent(in), | dimension(6) | :: | rv | ||
| class(reference_frame), | intent(inout) | :: | to | |||
| real(kind=wp), | intent(in) | :: | et |
the time of the transformation [sec] |
||
| class(ephemeris_class), | intent(inout) | :: | eph |
for ephemeris computations (assumed to have already been initialized) |
||
| real(kind=wp), | intent(out), | dimension(6) | :: | rv_out | ||
| logical, | intent(out) | :: | status_ok |
returns the state of the frame center w.r.t. the frame primary body.
| Type | Intent | Optional | Attributes | Name | ||
|---|---|---|---|---|---|---|
| class(two_body_rotating_frame), | intent(in) | :: | me | |||
| class(ephemeris_class), | intent(inout) | :: | eph |
for ephemeris computations (assumed to have already been initialized) |
||
| real(kind=wp), | intent(in) | :: | et |
ephemeris time [sec] |
||
| real(kind=wp), | intent(out), | dimension(6) | :: | rc |
state of frame center w.r.t. primary body [inertial] |
|
| logical, | intent(out) | :: | status_ok |
true if no errors. |
rotation matrix for ROTATING_PULSATING <-> ICRF
| Type | Intent | Optional | Attributes | Name | ||
|---|---|---|---|---|---|---|
| class(two_body_rotating_pulsating_frame), | intent(inout) | :: | me | |||
| class(ephemeris_class), | intent(inout) | :: | eph |
for ephemeris computations (assumed to have already been initialized) |
||
| logical, | intent(in) | :: | to_icrf | |||
| real(kind=wp), | intent(out), | dimension(3,3) | :: | c | ||
| real(kind=wp), | intent(out), | optional, | dimension(3,3) | :: | cdot | |
| logical, | intent(out) | :: | status_ok |
type,extends(two_body_rotating_frame),public :: two_body_rotating_pulsating_frame !! This frame is an extension of the two-body rotating frame, where !! a scale factor is used to scale the position and velocity of the state !! based on the distance between the primary and secondary bodies. real(wp) :: scale = zero !! scale factor contains procedure :: get_c_cdot => get_c_cdot_two_body_rotating_pulsating end type two_body_rotating_pulsating_frame