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OpenSpace/include/openspace/util/spicemanager.h
2015-06-26 19:20:56 +02:00

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/*****************************************************************************************
* *
* OpenSpace *
* *
* Copyright (c) 2014-2015 *
* *
* 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 *
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* 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 *
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* CONTRACT, TORT OR OTHERWISE, ARISING FROM, OUT OF OR IN CONNECTION WITH THE SOFTWARE *
* OR THE USE OR OTHER DEALINGS IN THE SOFTWARE. *
****************************************************************************************/
#ifndef __SPICEMANAGER_H__
#define __SPICEMANAGER_H__
#include "SpiceUsr.h"
#include "SpiceZpr.h"
#include <openspace/util/powerscaledcoordinate.h>
#include <ghoul/glm.h>
#include <ghoul/designpattern/singleton.h>
#include <glm/gtc/type_ptr.hpp>
#include <array>
#include <map>
#include <string>
#include <vector>
#include <set>
namespace openspace {
class SpiceManager : public ghoul::Singleton<SpiceManager> {
friend class ghoul::Singleton<SpiceManager>;
public:
typedef std::array<double, 36> TransformMatrix;
typedef unsigned int KernelIdentifier;
static const KernelIdentifier KernelFailed = KernelIdentifier(-1);
/**
* Loads one or more SPICE kernels into a program. The provided path can either be a
* binary, text-kernel, or meta-kernel which gets loaded into the kernel pool. The
* loading is done by passing the <code>filePath</code> to the <code>furnsh_c</code>
* function. http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/cspice/furnsh_c.html
* \param filePath The path to the kernel that should be loaded
* \return The loaded kernel's unique identifier that can be used to unload the kernel
*/
KernelIdentifier loadKernel(const std::string& filePath);
/**
* Function to find and store the intervals covered by a ck file, this is done
* by using mainly the <code>ckcov_c</code> and <code>ckobj_c</code> functions.
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/cspice/ckobj_c.html ,
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/cspice/ckcov_c.html
* \param filePath The path to the kernel that should be examined
* \return true if the operation was successful
*/
bool findCkCoverage(const std::string& path);
/**
* Function to find and store the intervals covered by a spk file, this is done
* by using mainly the <code>spkcov_c</code> and <code>spkobj_c</code> functions.
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/cspice/spkobj_c.html ,
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/cspice/spkcov_c.html
* \param filePath The path to the kernel that should be examined
* \return true if the operation was successful
*/
bool findSpkCoverage(const std::string& path);
/**
* \return true if SPK kernels have been loaded to cover <code>target</code>
* for time <code>et</code>
* \param target, the body to be examined
* \param et, the time when body is possibly covered
*/
bool hasSpkCoverage(std::string target, double& et) const;
/**
* \return true if CK kernels have been loaded to cover <code>frame</code>
* for time <code>et</code>
* \param frame, the frame to be examined
* \param et, the time when frame is possibly covered
*/
bool hasCkCoverage(std::string frame, double& et) const;
/**
* Unloads a SPICE kernel identified by the <code>kernelId</code> which was returned
* by the loading call to loadKernel. The unloading is done by calling the
* <code>unload_c</code> function.
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/cspice/unload_c.html.
* \param kernelId The unique identifier that was returned from the call to
* loadKernel which loaded the kernel
*/
void unloadKernel(KernelIdentifier kernelId);
/**
* Unloads a SPICE kernel identified by the <code>filePath</code> which was used in
* the loading call to loadKernel. The unloading is done by calling the
* <code>unload_c</code> function.
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/cspice/unload_c.html.
* \param filePath The path of the kernel that should be unloaded, it has to refer to
* a file that was loaded in using the loadKernel method
*/
void unloadKernel(const std::string& filePath);
/**
* Determines whether values exist for some <code>item</code> for any body,
* identified by it's <code>naifId</code>, in the kernel pool by passing it to the
* <code>bodfnd_c</code> function.
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/cspice/bodfnd_c.html
* For a description on NAIF IDs, see
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/req/naif_ids.html.
* \param naifId NAIF ID code of body
* \param item The item to find
* \return <code>true</code> if the function succeeded, <code>false</code> otherwise
*/
bool hasValue(int naifId, const std::string& item) const;
/**
* Determines whether values exist for some <code>item</code> for any
* <code>body</code> in the kernel pool by passing it to the <code>bodfnd_c</code>
* function.
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/cspice/bodfnd_c.html
* \param body The name of the body that should be sampled
* \param item The item to find
* \return <code>true</code> if the function succeeded, <code>false</code> otherwise
*/
bool hasValue(const std::string& body, const std::string& item) const;
/**
* Returns the NAIF ID for a specific body. For a description on NAIF IDs, see
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/req/naif_ids.html. The
* <code>id</code> will only be set if the retrieval was successful, otherwise it will
* remain unchanged.
* \param body The body name that should be retrieved
* \param id The ID of the <code>body</code> will be stored in this variable. The
* value will only be changed if the retrieval was successful
* \return <code>true</code> if the <code>body</code> was found, <code>false</code>
* otherwise
*/
bool getNaifId(const std::string& body, int& id) const;
/**
* Returns the NAIF ID for a specific frame using namfrm_c(), see
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/cspice/namfrm_c.html.
* The <code>id</code> will only be set if the retrieval was successful,
* otherwise it will remain unchanged.
* \param frame The frame name that should be retrieved
* \param id The ID of the <code>frame</code> will be stored in this variable. The
* value will only be changed if the retrieval was successful
* \return <code>true</code> if the <code>frame</code> was found, <code>false</code>
* otherwise
*/
bool getFrameId(const std::string& frame, int& id) const;
/**
* Retrieves a single <code>value</code> for a certain <code>body</code>. This method
* succeeds iff <code>body</code> is the name of a valid body, <code>value</code>
* is a value associated with the body, and the value consists of only a single
* <code>double</code> value. If all conditions are true, the value is retrieved using
* the method <code>bodvrd_c</code> and stored in <code>v</code>
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/cspice/bodvrd_c.html. If one of
* the conditions is false an error is logged and the value <code>v</code> is
* unchanged. For a description on NAIF IDs, see
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/req/naif_ids.html.
* \param body The name of the body whose value should be retrieved or the NAIF ID of
* this body
* \param value The value of that should be retrieved, this value is case-sensitive
* \param v The destination for the retrieved value
* \return <code>true</code> if the <code>body</code> named a valid body,
* <code>value</code> is a valid item for the <code>body</code> and the retrieved
* value is only a single value. <code>false</code> otherwise
*/
bool getValue(const std::string& body, const std::string& value, double& v) const;
/**
* Retrieves a <code>value</code> with three components for a certain
* <code>body</code>. This method succeeds iff <code>body</code> is the name of a
* valid body, <code>value</code> is a value associated with the body, and the value
* consists of three <code>double</code> values. If all conditions are true, the value
* is retrieved using the method <code>bodvrd_c</code> and stored in <code>v</code>
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/cspice/bodvrd_c.html. If one of
* the conditions is false an error is logged and the value <code>v</code> is
* unchanged. For a description on NAIF IDs, see
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/req/naif_ids.html.
* \param body The name of the body whose value should be retrieved or the NAIF ID of
* the body
* \param value The value of that should be retrieved, this value is case-sensitive
* \param v The destination for the retrieved values
* \return <code>true</code> if the <code>body</code> named a valid body,
* <code>value</code> is a valid item for the <code>body</code> and the retrieved
* value is only a single value. <code>false</code> otherwise
*/
bool getValue(const std::string& body, const std::string& value, glm::dvec3& v) const;
/**
* Retrieves a <code>value</code> with four components for a certain
* <code>body</code>. This method succeeds iff <code>body</code> is the name of a
* valid body, <code>value</code> is a value associated with the body, and the value
* consists of four <code>double</code> values. If all conditions are true, the value
* is retrieved using the method <code>bodvrd_c</code> and stored in <code>v</code>
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/cspice/bodvrd_c.html. If one of
* the conditions is false an error is logged and the value <code>v</code> is
* unchanged. For a description on NAIF IDs, see
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/req/naif_ids.html.
* \param body The name of the body whose value should be retrieved or the NAIF ID of
* the body
* \param value The value of that should be retrieved, this value is case-sensitive
* \param v The destination for the retrieved values
* \return <code>true</code> if the <code>body</code> named a valid body,
* <code>value</code> is a valid item for the <code>body</code> and the retrieved
* value is only a single value. <code>false</code> otherwise
*/
bool getValue(const std::string& body, const std::string& value, glm::dvec4& v) const;
/**
* Retrieves a <code>value</code> with an arbitrary number of components for a certain
* <code>body</code>. This method succeeds <code>body</code> is a valid body,
* <code>value</code> is a value associated with the body, and the value consists of a
* number of <code>double</code> values. The requested number is equal to the
* <code>size</code> of the passed vector <code>v</code> which means that this vector
* has to be preallocated. If all conditions are true, the value is retrieved using
* the method <code>bodvrd_c</code> and stored in <code>v</code>
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/cspice/bodvrd_c.html. If one of
* the conditions is false an error is logged and the value <code>v</code> is
* unchanged. For a description on NAIF IDs, see
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/req/naif_ids.html.
* \param body The body whose information should be retrieved or the NAIF ID of that
* body
* \param value The value of that should be retrieved, this value is case-sensitive
* \param v The destination for the retrieved values. The size of this vector
* determines how many values will be retrieved
* \return <code>true</code> if the <code>body</code> named a valid body,
* <code>value</code> is a valid item for the <code>body</code> and the retrieved
* value is only a single value. <code>false</code> otherwise
*/
bool getValue(const std::string& body, const std::string& value,
std::vector<double>& v) const;
bool spacecraftClockToET(const std::string& craftIdCode, double& craftTicks, double& et);
/**
* Converts the <code>timeString</code> representing a date to a double precision
* value representing the <code>ephemerisTime</code>; that is the number of TDB
* seconds past the J2000 epoch. For further details, please refer to
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/cspice/str2et_c.html. If an error
* occurs, an error is logged, the method returns <code>false</code> and the
* <code>ephemerisTime</code> remains unchanged.
* \param timeString A string representing the time to be converted
* \param ephemerisTime The destination for the converted time; the number of TDB
* seconds past the J2000 epoch, representing the passed <code>epochString</code>
* \return <code>true</code> if the <code>epochString</code> is a valid string and
* the conversion succeeded, <code>false</code> otherwise
*/
bool getETfromDate(const std::string& timeString, double& ephemerisTime) const;
/**
* Converts the passed <code>ephemerisTime</code> into a human-readable
* <code>date</code> string with a specific <code>format</code>. For details on the
* formatting, refer to
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/cspice/timout_c.html. In case of
* an error, <code>date</code> will not be modified, an error will be logged and the
* method returns <code>false</code>.
* \param ephemerisTime The ephemeris time, that is the number of TDB seconds past the
* J2000 epoch
* \param date The destination for the converted date. This will only be changed if
* the conversion succeeded
* \param format The format string describing the output format for the
* <code>date</code>
* \return <code>true</code> if the conversion succeeded, <code>false</code> otherwise
*/
bool getDateFromET(double ephemerisTime, std::string& date,
const std::string& format = "YYYY MON DDTHR:MN:SC.### ::RND") const;
/**
* Returns the <code>position</code> of a <code>target</code> body relative to an
* <code>observer</code> in a specific <code>referenceFrame</code>, optionally
* corrected for light time (planetary aberration) and stellar aberration
* (<code>aberrationCorrection</code>). For further details, refer to
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/cspice/spkpos_c.html. For more
* information on NAIF IDs, refer to
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/req/naif_ids.html
* \param target The target body name or the target body's NAIF ID
* \param observer The observing body name or the observing body's NAIF ID
* \param referenceFrame The reference frame of the output position vector
* \param aberrationCorrection The aberration correction flag out of the list of
* values (<code>NONE</code>, <code>LT</code>, <code>LT+S</code>, <code>CN</code>,
* <code>CN+S</code> for the reception case or <code>XLT</code>, <code>XLT+S</code>,
* <code>XCN</code>, or <code>XCN+S</code> for the transmission case.
* \param ephemerisTime The time at which the position is to be queried
* \param position The output containing the position of the target; if the method
* fails, the target position is unchanged
* \param lightTime If the <code>aberrationCorrection</code> is different from
* <code>NONE</code>, this variable will contain the one-way light time between the
* observer and the target. If the method fails, the lightTime is unchanged
* \return <code>true</code> if the function was successful, <code>false</code>
* otherwise
*/
bool getTargetPosition(const std::string& target,
const std::string& observer,
const std::string& referenceFrame,
const std::string& aberrationCorrection,
double ephemerisTime,
glm::dvec3& position,
double& lightTime) const;
bool getTargetPosition(const std::string& target,
const std::string& observer,
const std::string& referenceFrame,
const std::string& aberrationCorrection,
double ephemerisTime,
psc& position,
double& lightTime) const;
/**
* If a position is requested for an uncovered time in the SPK kernels,
* this function will insert a position in <code>modelPosition</code>.
* If the coverage has not yet started, the first position will be retrieved,
* If the coverage has ended, the last position will be retrieved
* If <code>time</code> is in a coverage gap, the position will be interpolated
* \param time, for which an estimated position is desirable
* \param target, the body which is missing SPK data for this time
* \param origin, the observer, the position will be retrieved in relation to this body
* \param modelPosition, the position of the body, passed by reference
* \return true if an estimated position is found
*/
bool getEstimatedPosition(const double time, const std::string target, const std::string origin, psc& modelPosition) const;
/**
* This helper method converts a 3 dimensional vector from one reference frame to another.
* \param v The vector to be converted
* \param from The frame to be converted from
* \param to The frame to be converted to
* \param ephemerisTime Time at which to get rotational matrix that transforms vector
* \return <code>true</code> if the conversion succeeded, <code>false</code> otherwise
*/
bool frameConversion(glm::dvec3& v, const std::string& from, const std::string& to, double ephemerisTime) const;
/**
* Finds the projection of one vector onto another vector.
* All vectors are 3-dimensional.
* \param v1 The vector to be projected.
* \param v2 The vector onto which v1 is to be projected.
* \return The projection of v1 onto v2.
*/
glm::dvec3 orthogonalProjection(glm::dvec3& v1, glm::dvec3& v2);
/**
* Given an observer and a direction vector defining a ray, compute
* the surface intercept of the ray on a target body at a specified
* epoch, optionally corrected for light time and stellar
* aberration.
* \param target Name of target body.
* \param observer Name of observing body.
* \param fovFrame Reference frame of ray's direction vector.
* \param bodyFixedFrame Body-fixed, body-centered target body frame.
* \param method Computation method.
* \param aberrationCorrection Aberration correction.
* \param ephemerisTime Epoch in ephemeris seconds past J2000 TDB.
* \param targetEpoch Intercept epoch.
* \param directionVector Ray's direction vector.
* \param surfaceIntercept Surface intercept point on the target body.
* \param surfaceVector Vector from observer to intercept point.
* \param isVisible Flag indicating whether intercept was found.
* \return <code>true</code> if not error occurred, <code>false</code> otherwise
* For further details, refer to
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/cspice/sincpt_c.html
*/
bool getSurfaceIntercept(const std::string& target,
const std::string& observer,
const std::string& fovFrame,
const std::string& bodyFixedFrame,
const std::string& method,
const std::string& aberrationCorrection,
double ephemerisTime,
double& targetEpoch,
glm::dvec3& directionVector,
glm::dvec3& surfaceIntercept,
glm::dvec3& surfaceVector,
bool& isVisible
) const;
/**
* Determine if a specified ephemeris object is within the
* field-of-view (FOV) of a specified instrument at a given time.
* \param instrument Name or ID code string of the instrument.
* \param target Name or ID code string of the target.
* \param observer Name or ID code string of the observer.
* \param aberrationCorrection Aberration correction method.
* \param method Type of shape model used for the target.
* \param referenceFrame Body-fixed, body-centered frame for target body.
* \param targetEpoch Time of the observation (seconds past J2000).
* \param isVisible <code>true</code> if the target is visible
* \return The success of the function
* For further detail, refer to
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/cspice/fovtrg_c.html
*/
bool targetWithinFieldOfView(const std::string& instrument,
const std::string& target,
const std::string& observer,
const std::string& method,
const std::string& referenceFrame,
const std::string& aberrationCorrection,
double& targetEpoch,
bool& isVisible
) const;
/**
* This method performs the same computation as the function its overloading
* with the exception that in doing so it assumes the inertial bodyfixed frame
* is that of 'IAU' type, allowing the client to omitt the
* <code>referenceFrame</code> for planetary objects.
*/
bool targetWithinFieldOfView(const std::string& instrument,
const std::string& target,
const std::string& observer,
const std::string& method,
const std::string& aberrationCorrection,
double& targetEpoch,
bool& isVisible
) const;
/**
* Returns the state vector (<code>position</code> and <code>velocity</code>) of a
* <code>target</code> body relative to an <code>observer</code> in a specific
* <code>referenceFrame</code>, optionally corrected for light time (planetary
* aberration) and stellar aberration (<code>aberrationCorrection</code>). For further
* details, refer to
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/cspice/spkezr_c.html. For more
* information on NAIF IDs, refer to
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/req/naif_ids.html
* \param target The target body name or the target body's NAIF ID
* \param observer The observing body name or the observing body's NAIF ID
* \param referenceFrame The reference frame of the output position vector
* \param aberrationCorrection The aberration correction flag out of the list of
* values (<code>NONE</code>, <code>LT</code>, <code>LT+S</code>, <code>CN</code>,
* <code>CN+S</code> for the reception case or <code>XLT</code>, <code>XLT+S</code>,
* <code>XCN</code>, or <code>XCN+S</code> for the transmission case.
* \param ephemerisTime The time at which the position is to be queried
* \param position The output containing the position of the target; if the method
* fails, the position is unchanged
* \param velocity The output containing the velocity of the target; if the method
* fails, the velocity is unchanged
* \param lightTime If the <code>aberrationCorrection</code> is different from
* <code>NONE</code>, this variable will contain the one-way light time between the
* observer and the target.If the method fails, the lightTime is unchanged
* \return <code>true</code> if the function was successful, <code>false</code>
* otherwise
*/
bool getTargetState(const std::string& target,
const std::string& observer,
const std::string& referenceFrame,
const std::string& aberrationCorrection,
double ephemerisTime,
glm::dvec3& position,
glm::dvec3& velocity,
double& lightTime) const;
bool getTargetState(const std::string& target,
const std::string& observer,
const std::string& referenceFrame,
const std::string& aberrationCorrection,
double ephemerisTime,
PowerScaledCoordinate& position,
PowerScaledCoordinate& velocity,
double& lightTime) const;
/**
* Returns the state transformation matrix used to convert from one frame to another
* at a specified <code>ephemerisTime</code>. For further details, please refer to
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/cspice/sxform_c.html.
* \param sourceFrame The name of the source reference frame
* \param destinationFrame The name of the destination reference frame
* \param ephemerisTime The time at which the transformation matrix is to be queried
* \param transformationMatrix The output containing the TransformMatrix containing
* the transformation matrix that defines the transformation from the
* <code>sourceFrame</code> to the <code>destinationFrame</code>. If the method fails
* the <code>transformationMatrix</code> is unchanged
* \return <code>true</code> if the function was successful, <code>false</code>
* otherwise
*/
bool getStateTransformMatrix(const std::string& sourceFrame,
const std::string& destinationFrame,
double ephemerisTime,
TransformMatrix& transformationMatrix) const;
/**
* Returns the matrix that transforms position vectors from one reference frame to
* another at a specified <code>ephemerisTime</code>. For further details, please refer to
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/cspice/pxform_c.html.
* \param sourceFrame The name of the source reference frame
* \param destinationFrame The name of the destination reference frame
* \param ephemerisTime The time at which the transformation matrix is to be queried
* \param transformationMatrix The output containing the transformation matrix that
* defines the transformation from the <code>sourceFrame</code> to the
* <code>destinationFrame</code>. If the method fails the
* <code>transformationMatrix</code> is unchanged
* \return <code>true</code> if the function was successful, <code>false</code>
* otherwise
*/
bool getPositionTransformMatrix(const std::string& sourceFrame,
const std::string& destinationFrame,
double ephemerisTime,
glm::dmat3& transformationMatrix) const;
/**
* The following overloaded function performs similar to its default - the exception being
* that it computes <code>transformationMatrix</code> with respect to local time offset
* between an observer and its target. This allows for the accountance of light travel of
* photons, e.g to account for instrument pointing offsets due to said phenomenon.
* \param sourceFrame The name of the source reference frame
* \param destinationFrame The name of the destination reference frame
* \param ephemerisTimeFrom Recorded/observed observation time
* \param ephemerisTimeTo Emission local target-time
* \param transformationMatrix The output containing the transformation matrix that
*/
bool getPositionTransformMatrix(const std::string& sourceFrame,
const std::string& destinationFrame,
double ephemerisTimeFrom,
double ephemerisTimeTo,
glm::dmat3& transformationMatrix) const;
/**
* If a transform matrix is requested for an uncovered time in the CK kernels,
* this function will insert a transform matrix in <code>positionMatrix</code>.
* If the coverage has not yet started, the first transform matrix will be retrieved,
* If the coverage has ended, the last transform matrix will be retrieved
* If <code>time</code> is in a coverage gap, the transform matrix will be interpolated
* \param time, for which an estimated transform matrix is desirable
* \param fromFrame, the transform matrix will be retrieved in relation to this frame
* \param toFrame, the frame missing CK data for this time
* \param positionMatrix, the estimated transform matrix of the frame, passed by reference
* \return true if an estimated transform matrix is found
*/
bool getEstimatedTransformMatrix(const double time, const std::string fromFrame, const std::string toFrame, glm::dmat3& positionMatrix) const;
/**
* Applies the <code>transformationMatrix</code> retrieved from
* getStateTransformMatrix to the <code>position</code> and <code>velocity</code>. The
* <code>position</code> and <code>velocity</code> parameters are used as input and
* output.
* \param position The position that should be transformed. The transformed position
* will be stored back in this parameter
* \param velocity The velocity that should be transformed. The transformed velocity
* will be stored back in this parameter
* \param transformationMatrix The 6x6 transformation matrix retrieved from
* getStateTransformMatrix that is used to transform the <code>position</code> and
* <code>velocity</code> vectors
*/
void applyTransformationMatrix(glm::dvec3& position,
glm::dvec3& velocity,
const TransformMatrix& transformationMatrix);
/**
* This routine returns the field-of-view (FOV) parameters for a specified
* <code>instrument</code>. For further details, please refer to
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/cspice/getfov_c.html.
* \param instrument The name of the instrument for which the FOV is to be retrieved
* \param fovShape The output containing the rough shape of the returned FOV. If the
* method fails, this value remains unchanged
* \param frameName The output containing the name of the frame in which the FOV
* <code>bounds</code> are computed. If the method fails, this value remains unchanged
* \param boresightVector The output containing the boresight, that is the vector for
* the center direction of the FOV. If the method fails, this value remains unchanged
* \param bounds The output containing the values defining the bounds of the FOV as
* explained by http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/cspice/getfov_c.html.
* If the method fails, this value remains unchanged
* \return <code>true</code> if the function was successful, <code>false</code>
* otherwise
*/
bool getFieldOfView(const std::string& instrument,
std::string& fovShape,
std::string& frameName,
glm::dvec3& boresightVector,
std::vector<glm::dvec3>& bounds) const;
/**
* This routine returns the field-of-view (FOV) parameters for a specified
* <code>instrument</code>. For further details, please refer to
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/cspice/getfov_c.html.
* \param instrument The NAIF id of the instrument for which the FOV is to be
* retrieved. For more information on NAIF IDs, refer to
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/req/naif_ids.html
* \param fovShape The output containing the rough shape of the returned FOV. If the
* method fails, this value remains unchanged
* \param frameName The output containing the name of the frame in which the FOV
* <code>bounds</code> are computed. If the method fails, this value remains unchanged
* \param boresightVector The output containing the boresight, that is the vector for
* the center direction of the FOV. If the method fails, this value remains unchanged
* \param bounds The output containing the values defining the bounds of the FOV as
* explained by http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/cspice/getfov_c.html.
* If the method fails, this value remains unchanged
* \return <code>true</code> if the function was successful, <code>false</code>
* otherwise
*/
bool getFieldOfView(int instrument, std::string& fovShape, std::string& frameName,
glm::dvec3& boresightVector, std::vector<glm::dvec3>& bounds) const;
/**
* This routine computes a set of points on the umbral or penumbral terminator of
* a specified target body, where SPICE models the target shape as an ellipsoid.
* \param numberOfPoints - number of points along terminator returned by this method
* \param terminatorType - is a string indicating the type of terminator to compute:
* umbral or penumbral. The umbral terminator is the boundary of the portion of the
* ellipsoid surface in total shadow. The penumbral terminator is the boundary of
* the portion of the surface that is completely illuminated. Note that in astronomy
* references, the unqualified word "terminator" refers to the umbral terminator.
* Here, the unqualified word refers to either type of terminator.
* \param lightSource - name of body acting as light source
* \param observer - name of bodserving body
* \param target - name of target body
* \param frame - name of the reference frame relative to which the output terminator
* points are expressed.
* \param aberrationCorrection - correction for light time and/or stellar aberration
* \param ephemerisTime - the epoch of participation of the observer
* \param targetEpoch - is the "target epoch.", time it takes for
* \param observerPosition - is the vector from the target body at targetEpoch
* \param terminatorPoints - an array of points on the umbral or penumbral terminator
* of the ellipsoid, as specified by the input argument `numberOfPoints'
* For further, more specific details please refer to
* http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/cspice/edterm_c.html
*/
bool getTerminatorEllipse(const int numberOfPoints,
const std::string terminatorType,
const std::string lightSource,
const std::string observer,
const std::string target,
const std::string frame,
const std::string aberrationCorrection,
double ephemerisTime,
double& targetEpoch,
glm::dvec3& observerPosition,
std::vector<psc>& terminatorPoints);
/**
* This function adds a frame to a body
* \param body - the name of the body
* \param frame - the name of the frame
* \return false if the arguments are empty
*/
bool addFrame(const std::string body, const std::string frame);
/**
* This function returns the frame of a body if defined, otherwise it returns
* IAU_ + body (most frames are known by the International Astronomical Union)
* \param body - the name of the body
* \return the frame of the body
*/
std::string frameFromBody(const std::string body) const;
/**
* This method checks if one of the previous SPICE methods has failed. If it has, the
* <code>errorMessage</code> is used to log an error along with the original SPICE
* error message.
* \param errorMessage The error message that will be logged if the method fails. If
* the argument is empty, no error message will be logged
* \return <code>true</code> if an error occurred, <code>false</code> otherwise
*/
static bool checkForError(std::string errorMessage);
/**
* This method uses the SPICE kernels to get the radii of bodies defined as a
* triaxial ellipsoid. The benefit of this is to be able to create more accurate
* planet shapes, which is desirable when projecting images with SPICE intersection
* methods
* \param planetName - the name of the body, should be recognizable by SPICE
* \param a - equatorial radius 1
* \param b - equatorial radius 2
* \param c - polar radius
* \return <code>true</code> if SPICE reports no errors
*/
bool getPlanetEllipsoid(std::string planetName, float &a, float &b, float &c);
protected:
struct KernelInformation {
std::string path; /// The path from which the kernel was loaded
KernelIdentifier id; /// A unique identifier for each kernel
int refCount; /// How many parts loaded this kernel and are interested in it
};
SpiceManager();
SpiceManager(const SpiceManager& c) = delete;
SpiceManager& operator=(const SpiceManager& r) = delete;
SpiceManager(SpiceManager&& r) = delete;
~SpiceManager();
/// A list of all loaded kernels
std::vector<KernelInformation> _loadedKernels;
// Map: id, vector of pairs. Pair: Start time, end time;
std::map<int, std::vector< std::pair<double, double> > > _ckIntervals;
std::map<int, std::vector< std::pair<double, double> > > _spkIntervals;
std::map<int, std::set<double> > _ckCoverageTimes;
std::map<int, std::set<double> > _spkCoverageTimes;
// Vector of pairs: Body, Frame
std::vector< std::pair<std::string, std::string> > _frameByBody;
const static bool _showErrors = false;
/// The last assigned kernel-id, used to determine the next free kernel id
KernelIdentifier _lastAssignedKernel;
};
} // namespace openspace
#endif // __SPICEMANAGER_H__