From 1f5b79f6ee02141da4053c6e6bd99b3bd3e5ba94 Mon Sep 17 00:00:00 2001
From: Luc Maisonobe <luc@orekit.org>
Date: Wed, 23 Jul 2014 14:56:53 +0200
Subject: [PATCH] Added getMinDate and getMaxDate to rugged API.

---
 .../main/java/org/orekit/rugged/api/Rugged.java    | 14 ++++++++++++++
 .../rugged/utils/SpacecraftToObservedBody.java     | 14 ++++++++++++++
 2 files changed, 28 insertions(+)

diff --git a/core/src/main/java/org/orekit/rugged/api/Rugged.java b/core/src/main/java/org/orekit/rugged/api/Rugged.java
index 4782da90..35157417 100644
--- a/core/src/main/java/org/orekit/rugged/api/Rugged.java
+++ b/core/src/main/java/org/orekit/rugged/api/Rugged.java
@@ -362,6 +362,20 @@ 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
diff --git a/core/src/main/java/org/orekit/rugged/utils/SpacecraftToObservedBody.java b/core/src/main/java/org/orekit/rugged/utils/SpacecraftToObservedBody.java
index bad7398d..477f83a0 100644
--- a/core/src/main/java/org/orekit/rugged/utils/SpacecraftToObservedBody.java
+++ b/core/src/main/java/org/orekit/rugged/utils/SpacecraftToObservedBody.java
@@ -139,6 +139,20 @@ 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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