Skip to content
GitLab
Explore
Sign in
Register
Primary navigation
Search or go to…
Project
hmyOreCZML
Manage
Activity
Members
Labels
Plan
Issues
Issue boards
Milestones
Wiki
Code
Merge requests
Repository
Branches
Commits
Tags
Repository graph
Compare revisions
Snippets
Build
Pipelines
Jobs
Pipeline schedules
Artifacts
Deploy
Releases
Package Registry
Container Registry
Model registry
Operate
Environments
Terraform modules
Monitor
Incidents
Analyze
Value stream analytics
Contributor analytics
CI/CD analytics
Repository analytics
Model experiments
Help
Help
Support
GitLab documentation
Compare GitLab plans
Community forum
Contribute to GitLab
Provide feedback
Keyboard shortcuts
?
Snippets
Groups
Projects
Show more breadcrumbs
houmingyang
hmyOreCZML
Commits
2f1cf585
Commit
2f1cf585
authored
4 weeks ago
by
houmingyang
Browse files
Options
Downloads
Patches
Plain Diff
change the param for test the Issue 61 bug.
parent
5b243d7f
No related branches found
No related tags found
No related merge requests found
Pipeline
#7743
failed
4 weeks ago
Stage: build
Stage: test
Changes
1
Pipelines
4
Hide whitespace changes
Inline
Side-by-side
Showing
1 changed file
oreczml-tutorials/src/main/java/org/orekit/czml/intervisu/InterVisuSatExample.java
+3
-3
3 additions, 3 deletions
...n/java/org/orekit/czml/intervisu/InterVisuSatExample.java
with
3 additions
and
3 deletions
oreczml-tutorials/src/main/java/org/orekit/czml/intervisu/InterVisuSatExample.java
+
3
−
3
View file @
2f1cf585
...
@@ -83,15 +83,15 @@ public class InterVisuSatExample {
...
@@ -83,15 +83,15 @@ public class InterVisuSatExample {
//// Build of the first satellite with an orbit with 20 degree inclination
//// Build of the first satellite with an orbit with 20 degree inclination
// Build of a LEO orbit
// Build of a LEO orbit
final
KeplerianOrbit
firstOrbit
=
new
KeplerianOrbit
(
78
7
8000
,
0
,
FastMath
.
toRadians
(
0
),
FastMath
.
toRadians
(
0
),
final
KeplerianOrbit
firstOrbit
=
new
KeplerianOrbit
(
78
3
8000
,
0
,
FastMath
.
toRadians
(
45
),
FastMath
.
toRadians
(
2
0
),
FastMath
.
toRadians
(
0
),
FastMath
.
toRadians
(
0
),
PositionAngleType
.
MEAN
,
FramesFactory
.
getEME2000
(),
startDate
,
FastMath
.
toRadians
(
0
),
FastMath
.
toRadians
(
0
),
PositionAngleType
.
MEAN
,
FramesFactory
.
getEME2000
(),
startDate
,
Constants
.
WGS84_EARTH_MU
);
Constants
.
WGS84_EARTH_MU
);
final
SpacecraftState
firstState
=
new
SpacecraftState
(
firstOrbit
);
final
SpacecraftState
firstState
=
new
SpacecraftState
(
firstOrbit
);
//// Build of the first satellite with an orbit with 40 degree inclination and omega of 90 degrees
//// Build of the first satellite with an orbit with 40 degree inclination and omega of 90 degrees
// Build of a LEO orbit
// Build of a LEO orbit
final
KeplerianOrbit
secondOrbit
=
new
KeplerianOrbit
(
70
78000
,
0
,
FastMath
.
toRadians
(
2
0
),
final
KeplerianOrbit
secondOrbit
=
new
KeplerianOrbit
(
178
78000
,
0
,
FastMath
.
toRadians
(
0
),
FastMath
.
toRadians
(
45
),
FastMath
.
toRadians
(
0
),
FastMath
.
toRadians
(
0
),
PositionAngleType
.
MEAN
,
FastMath
.
toRadians
(
120
),
FastMath
.
toRadians
(
0
),
FastMath
.
toRadians
(
0
),
PositionAngleType
.
MEAN
,
FramesFactory
.
getEME2000
(),
FramesFactory
.
getEME2000
(),
startDate
,
Constants
.
WGS84_EARTH_MU
);
startDate
,
Constants
.
WGS84_EARTH_MU
);
final
SpacecraftState
secondState
=
new
SpacecraftState
(
secondOrbit
);
final
SpacecraftState
secondState
=
new
SpacecraftState
(
secondOrbit
);
...
...
This diff is collapsed.
Click to expand it.
Preview
0%
Loading
Try again
or
attach a new file
.
Cancel
You are about to add
0
people
to the discussion. Proceed with caution.
Finish editing this message first!
Save comment
Cancel
Please
register
or
sign in
to comment