Commit d4a4ab55 authored by Luc Maisonobe's avatar Luc Maisonobe
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Whitespace.

parent 3b452765
...@@ -77,14 +77,14 @@ public interface PropulsionModel { ...@@ -77,14 +77,14 @@ public interface PropulsionModel {
T[] parameters); T[] parameters);
/** Get the mass derivative (i.e. flow rate in kg/s) during maneuver. /** Get the mass derivative (i.e. flow rate in kg/s) during maneuver.
*@param s current spacecraft state * @param s current spacecraft state
* @param parameters propulsion model parameters * @param parameters propulsion model parameters
* @return mass derivative in kg/s * @return mass derivative in kg/s
*/ */
double getMassDerivatives(SpacecraftState s, double[] parameters); double getMassDerivatives(SpacecraftState s, double[] parameters);
/** Get the mass derivative (i.e. flow rate in kg/s) during maneuver. /** Get the mass derivative (i.e. flow rate in kg/s) during maneuver.
*@param s current spacecraft state * @param s current spacecraft state
* @param parameters propulsion model parameters * @param parameters propulsion model parameters
* @param <T> extends CalculusFieldElement&lt;T&gt; * @param <T> extends CalculusFieldElement&lt;T&gt;
* @return mass derivative in kg/s * @return mass derivative in kg/s
......
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