From 43af43508553e0f35deaba6ff0c2270c7d1003f1 Mon Sep 17 00:00:00 2001 From: Henning Stahlke Date: Sun, 19 Nov 2017 11:20:46 +0100 Subject: [PATCH] YASIM: rename method getMAC to getMACLength --- src/FDM/YASim/Airplane.cpp | 8 ++++---- src/FDM/YASim/Wing.hpp | 2 +- src/FDM/YASim/yasim-test.cpp | 2 +- 3 files changed, 6 insertions(+), 6 deletions(-) diff --git a/src/FDM/YASim/Airplane.cpp b/src/FDM/YASim/Airplane.cpp index 22fc093a1..f25338830 100644 --- a/src/FDM/YASim/Airplane.cpp +++ b/src/FDM/YASim/Airplane.cpp @@ -320,7 +320,7 @@ float Airplane::compileWing(Wing* w) _wingsN->getNode("wing-area", true)->setFloatValue(w->getArea()); _wingsN->getNode("aspect-ratio", true)->setFloatValue(w->getAspectRatio()); _wingsN->getNode("standard-mean-chord", true)->setFloatValue(w->getSMC()); - _wingsN->getNode("mac", true)->setFloatValue(w->getMAC()); + _wingsN->getNode("mac", true)->setFloatValue(w->getMACLength()); _wingsN->getNode("mac-x", true)->setFloatValue(w->getMACx()); _wingsN->getNode("mac-y", true)->setFloatValue(w->getMACy()); } @@ -547,8 +547,8 @@ void Airplane::compile() aeroWgt += compileWing(_wing); // convert % to absolute x coordinates - _cgDesiredFront = _wing->getMACx() - _wing->getMAC()*_cgDesiredMin; - _cgDesiredAft = _wing->getMACx() - _wing->getMAC()*_cgDesiredMax; + _cgDesiredFront = _wing->getMACx() - _wing->getMACLength()*_cgDesiredMin; + _cgDesiredAft = _wing->getMACx() - _wing->getMACLength()*_cgDesiredMax; if (baseN != 0) { SGPropertyNode_ptr n = fgGetNode("/fdm/yasim/model", true); n->getNode("cg-x-range-front", true)->setFloatValue(_cgDesiredFront); @@ -1034,7 +1034,7 @@ float Airplane::getCGMAC() if (_wing) { float cg[3]; _model.getBody()->getCG(cg); - return (_wing->getMACx() - cg[0]) / _wing->getMAC(); + return (_wing->getMACx() - cg[0]) / _wing->getMACLength(); } return 0; } diff --git a/src/FDM/YASim/Wing.hpp b/src/FDM/YASim/Wing.hpp index d31d752c3..4cb26b051 100644 --- a/src/FDM/YASim/Wing.hpp +++ b/src/FDM/YASim/Wing.hpp @@ -78,7 +78,7 @@ public: float getArea() const { return _wingspan*_meanChord; }; float getAspectRatio() const { return _aspectRatio; }; float getSMC() const { return _meanChord; }; - float getMAC() const { return _mac; }; // get length of MAC + float getMACLength() const { return _mac; }; // get length of MAC float getMACx() const { return _macX; }; // get x-coord of MAC leading edge float getMACy() const { return _base[1]+_macRootDistance; }; // get y-coord of MAC leading edge diff --git a/src/FDM/YASim/yasim-test.cpp b/src/FDM/YASim/yasim-test.cpp index 8c4f69d63..d4f9f1518 100644 --- a/src/FDM/YASim/yasim-test.cpp +++ b/src/FDM/YASim/yasim-test.cpp @@ -248,7 +248,7 @@ int main(int argc, char** argv) float MAC = 0, MACx = 0, MACy = 0; Wing* wing = a->getWing(); if (wing) { - MAC = a->getWing()->getMAC(); + MAC = a->getWing()->getMACLength(); MACx = a->getWing()->getMACx(); MACy = a->getWing()->getMACy(); }