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== Impulsive maneuvers with orbital parameters criteriae == | == Impulsive maneuvers with orbital parameters criteriae == | ||
It is now possible to define an impulsive maneuver giving orbital parameters increments: | |||
* on semi-major axis | |||
* on eccentricity (and semi-major axis eventually) | |||
* on inclination (and semi-major axis eventually) | |||
== Recurrent date events == | == Recurrent date events == | ||
It is now possible to define date (relative or absolute ones) events with a recurrence (for example each day). | It is now possible to define date (relative or absolute ones) events with a recurrence (for example each day) using specific widgets as [{{PathCurrentJavaDoc}}/fr/cnes/genopus/events/GPRecurrentDateDetector.html GPRecurrentDateDetector] and [{{PathCurrentJavaDoc}}/fr/cnes/genopus/events/GPRecurrentRelativeDateDetector.html GPRecurrentRelativeDateDetector]. | ||
== New widget for numerical integrators definition == | == New widget for numerical integrators definition == | ||
New specific widgets have been created to deal with numerical integrators as some of ones defined in [http://patrius.cnes.fr PATRIUS]: <font color=#FF8C00>Runge Kutta 4</font>, <font color=#FF8C00>Runge Kutta 6</font> and <font color=#FF8C00>Dormand Price 853</font> | New specific widgets have been created to deal with numerical integrators as some of ones defined in [http://patrius.cnes.fr PATRIUS]: <font color=#FF8C00>Runge Kutta 4</font>, <font color=#FF8C00>Runge Kutta 6</font> and <font color=#FF8C00>Dormand Price 853</font>. More informations are given [http://genopus.cnes.fr/index.php/GPIntegrator here]. | ||
== Additional validity criteria on PRS coefficients == | == Additional validity criteria on PRS coefficients == | ||
Besides validity interval of [0,1] for each coefficient, there is an additional test on the sum of the three coefficients (absorption, specular and diffuse) that must be equal to 1. | Besides validity interval of [0,1] for each coefficient, there is an additional test on the sum of the three coefficients (absorption, specular and diffuse) that must be equal to 1. | ||
== New autonomous tool to work on orbit data == | == New autonomous tool to work on orbit data == | ||
For people who want to work on orbit characteristics (date, frame, parameters) without coding, it is now possible to use a dedicated autonomous tool with its own <font color=#FF8C00 title="Graphical User Interface">GUI</font> (gporbitconvertor-x.x-jar-with-dependencies.jar). | |||
== Anomaly corrections == | == Anomaly corrections == | ||
* Impossibility to initialize an orbit using a H0-n frame. | * Impossibility to initialize an orbit using a H0-n frame. | ||
* Bad [[https://logiciels.cnes.fr/en/node/62?type=desc PATRIUS]] <font color=#4169E1>Orbit</font> building when using the <font color=#4169E1>getPatriusObject()</font> method: if the displayed frame is different of the "pivot" one, displayed frame is taken into account but orbital elements are coming from the "pivot" one (this bug was also present in previous versions). | |||
* Calling [{{PathCurrentJavaDoc}}/fr/cnes/genopus/events/GPVisibilityFromStationDetector.html GPVisibilityFromStationDetector] or [{{PathCurrentJavaDoc}}/fr/cnes/genopus/attitudes/GPAttitudeSequence.html GPAttitudeSequence] widgets make the tool incompatible with a headless mode (no display). | * Calling [{{PathCurrentJavaDoc}}/fr/cnes/genopus/events/GPVisibilityFromStationDetector.html GPVisibilityFromStationDetector] or [{{PathCurrentJavaDoc}}/fr/cnes/genopus/attitudes/GPAttitudeSequence.html GPAttitudeSequence] widgets make the tool incompatible with a headless mode (no display). | ||
Dernière version du 8 novembre 2019 à 07:57
Compatibility with PATRIUS
This version is compatible with the version 4.4 of the PATRIUS library.
New Time scales
If the default mode is the same than for the previous versions, it is now possible to customize the time scales menu of the GPAbsoluteDate widget and thus to add these additional scales (available inside the PATRIUS library) as in the example below:
ts[0] = GPDateTimeScale.GMST;
ts[1] = GPDateTimeScale.GST;
ts[2] = GPDateTimeScale.TCG;
ts[3] = GPDateTimeScale.UTC;
gpDate = new GPAbsoluteDate("Date:", date0, ts);
New maneuvers trigerring criteriae
New criteriae on nodes and apsides have been added to the previous ones (relative or absolute dates and AOL)
Impulsive maneuvers with orbital parameters criteriae
It is now possible to define an impulsive maneuver giving orbital parameters increments:
- on semi-major axis
- on eccentricity (and semi-major axis eventually)
- on inclination (and semi-major axis eventually)
Recurrent date events
It is now possible to define date (relative or absolute ones) events with a recurrence (for example each day) using specific widgets as GPRecurrentDateDetector and GPRecurrentRelativeDateDetector.
New widget for numerical integrators definition
New specific widgets have been created to deal with numerical integrators as some of ones defined in PATRIUS: Runge Kutta 4, Runge Kutta 6 and Dormand Price 853. More informations are given here.
Additional validity criteria on PRS coefficients
Besides validity interval of [0,1] for each coefficient, there is an additional test on the sum of the three coefficients (absorption, specular and diffuse) that must be equal to 1.
New autonomous tool to work on orbit data
For people who want to work on orbit characteristics (date, frame, parameters) without coding, it is now possible to use a dedicated autonomous tool with its own GUI (gporbitconvertor-x.x-jar-with-dependencies.jar).
Anomaly corrections
- Impossibility to initialize an orbit using a H0-n frame.
- Bad [PATRIUS] Orbit building when using the getPatriusObject() method: if the displayed frame is different of the "pivot" one, displayed frame is taken into account but orbital elements are coming from the "pivot" one (this bug was also present in previous versions).
- Calling GPVisibilityFromStationDetector or GPAttitudeSequence widgets make the tool incompatible with a headless mode (no display).