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Ref T429, PBH interpolator
* make sure all angle interpolations interpolate "in the right direction" (like previously only for heaading) * one single function for angle interpolation
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@@ -8,7 +8,11 @@
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*/
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#include "interpolatorpbh.h"
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#include "interpolatorfunctions.h"
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#include "blackmisc/verify.h"
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#include "blackconfig/buildconfig.h"
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using namespace BlackConfig;
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using namespace BlackMisc::Aviation;
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using namespace BlackMisc::PhysicalQuantities;
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@@ -16,45 +20,49 @@ namespace BlackMisc
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{
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namespace Simulation
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{
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CAngle CInterpolatorPbh::interpolateAngle(const CAngle &begin, const CAngle &end, double timeFraction0to1)
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{
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// determine the right direction (to left, to right) we interpolate towards to
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// -30 -> 30 => 60 (via 0)
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// 30 -> -30 => -60 (via 0)
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// 170 -> -170 => -340 (via 180)
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// -170 -> 170 => 340 (via 180)
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double deltaDeg = (end - begin).value(CAngleUnit::deg());
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if (deltaDeg > 180.0) { deltaDeg -= 360; }
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else if (deltaDeg < -180.0) { deltaDeg += 360; }
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if (CBuildConfig::isLocalDeveloperDebugBuild())
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{
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BLACK_VERIFY_X(isValidTimeFraction(timeFraction0to1), Q_FUNC_INFO, "0..1 fraction needed");
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}
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return begin + CAngle(timeFraction0to1 * deltaDeg, CAngleUnit::deg());
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}
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CHeading CInterpolatorPbh::getHeading() const
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{
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// HINT: VTOL aircraft can change pitch/bank without changing position, planes cannot
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// Interpolate heading: HDG = (HdgB - HdgA) * t + HdgA
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const CHeading headingBegin = m_oldSituation.getHeading();
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CHeading headingEnd = m_newSituation.getHeading();
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const CHeading headingEnd = m_newSituation.getHeading();
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if ((headingEnd - headingBegin).value(CAngleUnit::deg()) < -180)
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if (CBuildConfig::isLocalDeveloperDebugBuild())
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{
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headingEnd += CHeading(360, CHeading::Magnetic, CAngleUnit::deg());
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BLACK_VERIFY_X(headingBegin.getReferenceNorth() == headingEnd.getReferenceNorth(), Q_FUNC_INFO, "Need same reference");
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}
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if ((headingEnd - headingBegin).value(CAngleUnit::deg()) > 180)
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{
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headingEnd -= CHeading(360, CHeading::Magnetic, CAngleUnit::deg());
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}
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return CHeading((headingEnd - headingBegin)
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* m_simulationTimeFraction
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+ headingBegin,
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headingBegin.getReferenceNorth());
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return CHeading(interpolateAngle(headingBegin, headingEnd, m_simulationTimeFraction), headingEnd.getReferenceNorth());
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}
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CAngle CInterpolatorPbh::getPitch() const
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{
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// Interpolate Pitch: Pitch = (PitchB - PitchA) * t + PitchA
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const CAngle pitchBegin = m_oldSituation.getPitch();
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const CAngle pitchEnd = m_newSituation.getPitch();
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const CAngle pitch = (pitchEnd - pitchBegin) * m_simulationTimeFraction + pitchBegin;
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return pitch;
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return interpolateAngle(m_oldSituation.getPitch(), m_newSituation.getPitch(), m_simulationTimeFraction);
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}
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CAngle CInterpolatorPbh::getBank() const
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{
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// Interpolate bank: Bank = (BankB - BankA) * t + BankA
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const CAngle bankBegin = m_oldSituation.getBank();
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const CAngle bankEnd = m_newSituation.getBank();
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const CAngle bank = (bankEnd - bankBegin) * m_simulationTimeFraction + bankBegin;
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return bank;
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return interpolateAngle(m_oldSituation.getBank(), m_newSituation.getBank(), m_simulationTimeFraction);
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}
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CSpeed CInterpolatorPbh::getGroundSpeed() const
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@@ -63,5 +71,20 @@ namespace BlackMisc
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* m_simulationTimeFraction
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+ m_oldSituation.getGroundSpeed();
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}
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void CInterpolatorPbh::setSituations(const CAircraftSituation &older, const CAircraftSituation &newer)
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{
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m_oldSituation = older;
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m_newSituation = newer;
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}
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void CInterpolatorPbh::setTimeFraction(double tf)
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{
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if (CBuildConfig::isLocalDeveloperDebugBuild())
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{
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BLACK_VERIFY_X(isValidTimeFraction(tf), Q_FUNC_INFO, "Time fraction needs to be 0-1");
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}
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m_simulationTimeFraction = clampValidTimeFraction(tf);
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}
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} // namespace
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} // namespace
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@@ -16,13 +16,14 @@
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#include "blackmisc/aviation/heading.h"
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#include "blackmisc/pq/angle.h"
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#include "blackmisc/pq/speed.h"
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#include "blackmisc/blackmiscexport.h"
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namespace BlackMisc
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{
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namespace Simulation
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{
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//! Simple interpolator for pitch, bank, heading, groundspeed
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class CInterpolatorPbh
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class BLACKMISC_EXPORT CInterpolatorPbh
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{
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public:
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//! Constructor
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@@ -42,10 +43,17 @@ namespace BlackMisc
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const Aviation::CAircraftSituation &getNewSituation() const { return m_newSituation; }
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//! @}
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//! Set situations
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//! \remark mostly needed for UNIT tests
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void setSituations(const Aviation::CAircraftSituation &older, const Aviation::CAircraftSituation &newer);
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//! Change time fraction
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void setTimeFraction(double tf) { m_simulationTimeFraction = tf; }
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void setTimeFraction(double tf);
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private:
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//! Interpolate angle
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static PhysicalQuantities::CAngle interpolateAngle(const PhysicalQuantities::CAngle &begin, const PhysicalQuantities::CAngle &end, double timeFraction0to1);
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double m_simulationTimeFraction = 0.0;
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Aviation::CAircraftSituation m_oldSituation;
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Aviation::CAircraftSituation m_newSituation;
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