Commit e74b8a59 by Luc Maisonobe

### Typos.

parent 6c2266ae
 ... ... @@ -27,7 +27,7 @@ import org.orekit.forces.maneuvers.trigger.ManeuverTriggersResetter; /** Generator for one column of a Jacobian matrix for special case of trigger dates. *

* Typical use cases for this are estimation of maneuver start and stop date during * either orbit determination or maneuver optimisation. * either orbit determination or maneuver optimization. *

*

* Let $$(t_0, y_0)$$ be the state at propagation start, $$(t_1, y_1)$$ be the state at ... ... @@ -49,7 +49,7 @@ import org.orekit.forces.maneuvers.trigger.ManeuverTriggersResetter; * respect to intermediate time $$t_1$$: * $\frac{\partial y_t}{\partial y_0} = \frac{\partial y_t}{\partial y_1} \frac{\partial y_1}{\partial y_0}$ * We deduce * $\frac{\partial y_t}{\partial y_1} = \frac{\partial y_t}{\partial y_0} \left(\frac{\partial y_1}{\partial y_0}\right)^{-1}$. * $\frac{\partial y_t}{\partial y_1} = \frac{\partial y_t}{\partial y_0} \left(\frac{\partial y_1}{\partial y_0}\right)^{-1}$ *

*

* The Jacobian column can therefore be computed using the following closed-form expression: ... ... @@ -62,7 +62,7 @@ import org.orekit.forces.maneuvers.trigger.ManeuverTriggersResetter; *

* As the column is generated using a closed-form expression, this generator implements * the {@link AdditionalStateProvider} interface and stores the column directly * in the premiary state during propagation. * in the primary state during propagation. *

*

* The implementation takes care to not resetting anything at propagation start. ... ...

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