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youngcle
Rugged-MOD
Commits
0d10404e
Commit
0d10404e
authored
10 years ago
by
Luc Maisonobe
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Merge branch 'master' of
ssh://git@www.orekit.org/rugged-main.git
parents
bbe32424
1f5b79f6
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2 changed files
core/src/main/java/org/orekit/rugged/api/Rugged.java
+15
-1
15 additions, 1 deletion
core/src/main/java/org/orekit/rugged/api/Rugged.java
core/src/main/java/org/orekit/rugged/utils/SpacecraftToObservedBody.java
+14
-0
14 additions, 0 deletions
...ava/org/orekit/rugged/utils/SpacecraftToObservedBody.java
with
29 additions
and
1 deletion
core/src/main/java/org/orekit/rugged/api/Rugged.java
+
15
−
1
View file @
0d10404e
...
...
@@ -366,6 +366,20 @@ public class Rugged {
return
sensors
.
values
();
}
/** Get the start of search time span.
* @return start of search time span
*/
public
AbsoluteDate
getMinDate
()
{
return
scToBody
.
getMinDate
();
}
/** Get the end of search time span.
* @return end of search time span
*/
public
AbsoluteDate
getMaxDate
()
{
return
scToBody
.
getMaxDate
();
}
/** Select inertial frame.
* @param inertialFrameId inertial frame identifier
* @return inertial frame
...
...
@@ -692,7 +706,7 @@ public class Rugged {
* @return selected sensor
* @exception RuggedException if sensor is not known
*/
p
rivate
LineSensor
getLineSensor
(
final
String
sensorName
)
throws
RuggedException
{
p
ublic
LineSensor
getLineSensor
(
final
String
sensorName
)
throws
RuggedException
{
final
LineSensor
sensor
=
sensors
.
get
(
sensorName
);
if
(
sensor
==
null
)
{
throw
new
RuggedException
(
RuggedMessages
.
UNKNOWN_SENSOR
,
sensorName
);
...
...
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core/src/main/java/org/orekit/rugged/utils/SpacecraftToObservedBody.java
+
14
−
0
View file @
0d10404e
...
...
@@ -164,6 +164,20 @@ public class SpacecraftToObservedBody {
}
}
/** Get the start of search time span.
* @return start of search time span
*/
public
AbsoluteDate
getMinDate
()
{
return
minDate
;
}
/** Get the end of search time span.
* @return end of search time span
*/
public
AbsoluteDate
getMaxDate
()
{
return
maxDate
;
}
/** Get transform from spacecraft to inertial frame.
* @param date date of the transform
* @return transform from spacecraft to inertial frame
...
...
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