YASim method name clarification Wing::setSpoiler
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ce753c0382
4 changed files with 6 additions and 6 deletions
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@ -215,7 +215,7 @@ void ControlMap::applyControls(float dt)
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case FLAP0EFFECTIVENESS: ((Wing*)obj)->setFlap0Effectiveness(lval); break;
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case FLAP0EFFECTIVENESS: ((Wing*)obj)->setFlap0Effectiveness(lval); break;
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case FLAP1: ((Wing*)obj)->setFlap1(lval, rval); break;
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case FLAP1: ((Wing*)obj)->setFlap1(lval, rval); break;
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case FLAP1EFFECTIVENESS: ((Wing*)obj)->setFlap1Effectiveness(lval); break;
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case FLAP1EFFECTIVENESS: ((Wing*)obj)->setFlap1Effectiveness(lval); break;
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case SPOILER: ((Wing*)obj)->setSpoiler(lval, rval); break;
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case SPOILER: ((Wing*)obj)->setSpoilerPos(lval, rval); break;
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case COLLECTIVE: ((Rotor*)obj)->setCollective(lval); break;
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case COLLECTIVE: ((Rotor*)obj)->setCollective(lval); break;
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case CYCLICAIL: ((Rotor*)obj)->setCyclicail(lval,rval); break;
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case CYCLICAIL: ((Rotor*)obj)->setCyclicail(lval,rval); break;
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case CYCLICELE: ((Rotor*)obj)->setCyclicele(lval,rval); break;
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case CYCLICELE: ((Rotor*)obj)->setCyclicele(lval,rval); break;
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@ -491,7 +491,7 @@ void FGFDM::startElement(const char* name, const XMLAttributes &atts)
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((Wing*)_currObj)->setSlat(attrf(a, "start"), attrf(a, "end"),
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((Wing*)_currObj)->setSlat(attrf(a, "start"), attrf(a, "end"),
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attrf(a, "aoa"), attrf(a, "drag"));
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attrf(a, "aoa"), attrf(a, "drag"));
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} else if(eq(name, "spoiler")) {
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} else if(eq(name, "spoiler")) {
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((Wing*)_currObj)->setSpoiler(attrf(a, "start"), attrf(a, "end"),
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((Wing*)_currObj)->setSpoilerParams(attrf(a, "start"), attrf(a, "end"),
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attrf(a, "lift"), attrf(a, "drag"));
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attrf(a, "lift"), attrf(a, "drag"));
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/* } else if(eq(name, "collective")) {
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/* } else if(eq(name, "collective")) {
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((Rotor*)_currObj)->setcollective(attrf(a, "min"), attrf(a, "max"));
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((Rotor*)_currObj)->setcollective(attrf(a, "min"), attrf(a, "max"));
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@ -159,7 +159,7 @@ void Wing::setSlat(float start, float end, float aoa, float drag)
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_slatDrag = drag;
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_slatDrag = drag;
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}
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}
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void Wing::setSpoiler(float start, float end, float lift, float drag)
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void Wing::setSpoilerParams(float start, float end, float lift, float drag)
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{
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{
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_spoilerStart = start;
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_spoilerStart = start;
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_spoilerEnd = end;
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_spoilerEnd = end;
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@ -209,7 +209,7 @@ void Wing::setFlap1Effectiveness(float lval)
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}
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}
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}
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}
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void Wing::setSpoiler(float lval, float rval)
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void Wing::setSpoilerPos(float lval, float rval)
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{
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{
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lval = Math::clamp(lval, 0, 1);
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lval = Math::clamp(lval, 0, 1);
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rval = Math::clamp(rval, 0, 1);
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rval = Math::clamp(rval, 0, 1);
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@ -35,13 +35,13 @@ public:
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void setFlap0(float start, float end, float lift, float drag);
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void setFlap0(float start, float end, float lift, float drag);
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void setFlap1(float start, float end, float lift, float drag);
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void setFlap1(float start, float end, float lift, float drag);
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void setSpoiler(float start, float end, float lift, float drag);
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void setSpoilerParams(float start, float end, float lift, float drag);
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void setSlat(float start, float end, float aoa, float drag);
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void setSlat(float start, float end, float aoa, float drag);
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// Set the control axes for the sub-surfaces
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// Set the control axes for the sub-surfaces
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void setFlap0(float lval, float rval);
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void setFlap0(float lval, float rval);
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void setFlap1(float lval, float rval);
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void setFlap1(float lval, float rval);
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void setSpoiler(float lval, float rval);
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void setSpoilerPos(float lval, float rval);
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void setSlat(float val);
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void setSlat(float val);
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void setFlap0Effectiveness(float lval);
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void setFlap0Effectiveness(float lval);
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void setFlap1Effectiveness(float lval);
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void setFlap1Effectiveness(float lval);
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