This commit is contained in:
Jonathan Fransson
2019-03-25 14:40:28 -06:00
7 changed files with 197 additions and 26 deletions
+5 -1
View File
@@ -29,6 +29,7 @@ set(HEADER_FILES
${CMAKE_CURRENT_SOURCE_DIR}/rendering/planetgeometry.h
${CMAKE_CURRENT_SOURCE_DIR}/rendering/renderableconstellationbounds.h
${CMAKE_CURRENT_SOURCE_DIR}/rendering/renderableplanet.h
${CMAKE_CURRENT_SOURCE_DIR}/rendering/renderablesatellites.h
${CMAKE_CURRENT_SOURCE_DIR}/rendering/renderablerings.h
${CMAKE_CURRENT_SOURCE_DIR}/rendering/renderablestars.h
${CMAKE_CURRENT_SOURCE_DIR}/rendering/simplespheregeometry.h
@@ -44,8 +45,9 @@ source_group("Header Files" FILES ${HEADER_FILES})
set(SOURCE_FILES
${CMAKE_CURRENT_SOURCE_DIR}/rendering/renderablesatellites.cpp
${CMAKE_CURRENT_SOURCE_DIR}/rendering/planetgeometry.cpp
${CMAKE_CURRENT_SOURCE_DIR}/rendering/renderableconstellationbounds.cpp
${CMAKE_CURRENT_SOURCE_DIR}/rendering/renderableconstellationbounds.cpp
${CMAKE_CURRENT_SOURCE_DIR}/rendering/renderableplanet.cpp
${CMAKE_CURRENT_SOURCE_DIR}/rendering/renderablesatellites.cpp
${CMAKE_CURRENT_SOURCE_DIR}/rendering/renderablerings.cpp
${CMAKE_CURRENT_SOURCE_DIR}/rendering/renderablestars.cpp
${CMAKE_CURRENT_SOURCE_DIR}/rendering/simplespheregeometry.cpp
@@ -62,6 +64,8 @@ set(SHADER_FILES
${CMAKE_CURRENT_SOURCE_DIR}/shaders/constellationbounds_vs.glsl
${CMAKE_CURRENT_SOURCE_DIR}/shaders/nighttexture_fs.glsl
${CMAKE_CURRENT_SOURCE_DIR}/shaders/nighttexture_vs.glsl
${CMAKE_CURRENT_SOURCE_DIR}/shaders/renderablekeplerorbits_fs.glsl
${CMAKE_CURRENT_SOURCE_DIR}/shaders/renderablekeplerorbits_vs.glsl
${CMAKE_CURRENT_SOURCE_DIR}/shaders/renderableplanet_fs.glsl
${CMAKE_CURRENT_SOURCE_DIR}/shaders/renderableplanet_vs.glsl
${CMAKE_CURRENT_SOURCE_DIR}/shaders/rings_vs.glsl
@@ -232,7 +232,6 @@ RenderableSatellites::RenderableSatellites(const ghoul::Dictionary& dictionary)
int lineNum = 1;
if (dictionary.hasKeyAndValue)<double>(KeyLineNum) {
lineNum = static_cast<int>(dictionary.value<double>(KeyLineNum));
}
readTLEFile(file, lineNum);
}
@@ -0,0 +1,46 @@
/*****************************************************************************************
* *
* OpenSpace *
* *
* Copyright (c) 2014-2018 *
* *
* Permission is hereby granted, free of charge, to any person obtaining a copy of this *
* software and associated documentation files (the "Software"), to deal in the Software *
* without restriction, including without limitation the rights to use, copy, modify, *
* merge, publish, distribute, sublicense, and/or sell copies of the Software, and to *
* permit persons to whom the Software is furnished to do so, subject to the following *
* conditions: *
* *
* The above copyright notice and this permission notice shall be included in all copies *
* or substantial portions of the Software. *
* *
* THE SOFTWARE IS PROVIDED "AS IS", WITHOUT WARRANTY OF ANY KIND, EXPRESS OR IMPLIED, *
* INCLUDING BUT NOT LIMITED TO THE WARRANTIES OF MERCHANTABILITY, FITNESS FOR A *
* PARTICULAR PURPOSE AND NONINFRINGEMENT. IN NO EVENT SHALL THE AUTHORS OR COPYRIGHT *
* HOLDERS BE LIABLE FOR ANY CLAIM, DAMAGES OR OTHER LIABILITY, WHETHER IN AN ACTION OF *
* CONTRACT, TORT OR OTHERWISE, ARISING FROM, OUT OF OR IN CONNECTION WITH THE SOFTWARE *
* OR THE USE OR OTHER DEALINGS IN THE SOFTWARE. *
****************************************************************************************/
#include "fragment.glsl"
#include "floatoperations.glsl"
uniform vec3 color;
uniform float opacity = 1.0;
uniform bool useLineFade;
uniform float lineFade;
in vec4 viewSpacePosition;
Fragment getFragment() {
Fragment frag;
frag.color = vec4(color, opacity);
frag.depth = safeLength(viewSpacePosition);
frag.blend = BLEND_MODE_ADDITIVE;
frag.gPosition = viewSpacePosition;
// There is no normal here
frag.gNormal = vec4(0.0, 0.0, -1.0, 1.0);
return frag;
}
@@ -0,0 +1,44 @@
/*****************************************************************************************
* *
* OpenSpace *
* *
* Copyright (c) 2014-2018 *
* *
* Permission is hereby granted, free of charge, to any person obtaining a copy of this *
* software and associated documentation files (the "Software"), to deal in the Software *
* without restriction, including without limitation the rights to use, copy, modify, *
* merge, publish, distribute, sublicense, and/or sell copies of the Software, and to *
* permit persons to whom the Software is furnished to do so, subject to the following *
* conditions: *
* *
* The above copyright notice and this permission notice shall be included in all copies *
* or substantial portions of the Software. *
* *
* THE SOFTWARE IS PROVIDED "AS IS", WITHOUT WARRANTY OF ANY KIND, EXPRESS OR IMPLIED, *
* INCLUDING BUT NOT LIMITED TO THE WARRANTIES OF MERCHANTABILITY, FITNESS FOR A *
* PARTICULAR PURPOSE AND NONINFRINGEMENT. IN NO EVENT SHALL THE AUTHORS OR COPYRIGHT *
* HOLDERS BE LIABLE FOR ANY CLAIM, DAMAGES OR OTHER LIABILITY, WHETHER IN AN ACTION OF *
* CONTRACT, TORT OR OTHERWISE, ARISING FROM, OUT OF OR IN CONNECTION WITH THE SOFTWARE *
* OR THE USE OR OTHER DEALINGS IN THE SOFTWARE. *
****************************************************************************************/
#version __CONTEXT__
layout(location = 0) in vec4 vertexData;
uniform dmat4 modelViewTransform;
uniform mat4 projectionTransform;
uniform bool useLineFade;
uniform float lineFade;
uniform int vertexSortingMethod;
uniform int pointSize;
out vec4 viewSpacePosition;
void main() {
dvec4 position = dvec4(vertexData.xyz, 1.0);
float timeOffset = vertexData.w;
viewSpacePosition = vec4(modelViewTransform * position);
gl_Position = projectionTransform * viewSpacePosition;
}
@@ -47,6 +47,27 @@ public:
std::string offender;
};
struct KeplerOrbit {
/// The period of the orbit in seconds
double period() const;
/// The eccentricity of the orbit in [0, 1)
double eccentricity;
/// The semi-major axis in km
double semiMajorAxis;
/// The inclination of the orbit in [0, 360]
double inclination;
/// The right ascension of the ascending node in [0, 360]
double ascendingNode;
/// The argument of periapsis in [0, 360]
double argumentOfPeriapsis;
/// The mean anomaly at the epoch in [0, 360]
double meanAnomalyAtEpoch;
/// The epoch in seconds relative to the J2000 epoch
double epoch;
/// The mass of the more massive body
double massiveBodyMass = 1.989E30; // Sun's mass in kg
};
/**
* The constructor that retrieves the required Keplerian elements from the passed
* \p dictionary. These values are then apssed to the setKeplerElements method for