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fix gcc warnings

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Mostly comment out unused variables.
This commit is contained in:
Tim Moore 2009-08-24 17:57:32 +02:00
parent 1e049f24b0
commit 5a1e0d92f4
2 changed files with 12 additions and 12 deletions
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14
src/FDM/YASim/Rotor.cpp
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@ -818,7 +818,7 @@ void Rotor::calcLiftFactor(float* v, float rho, State *s)
_f_ge=1+_diameter/_ground_effect_altitude*_ground_effect_constant; _f_ge=1+_diameter/_ground_effect_altitude*_ground_effect_constant;
// Now calculate translational lift // Now calculate translational lift
float v_vert = Math::dot3(v,_normal); // float v_vert = Math::dot3(v,_normal);
float help[3]; float help[3];
Math::cross3(v,_normal,help); Math::cross3(v,_normal,help);
float v_horiz = Math::mag3(help); float v_horiz = Math::mag3(help);
@ -1181,7 +1181,7 @@ void Rotor::compile()
* _diameter * _rel_blade_center * _rel_blade_center /(0.5*0.5); * _diameter * _rel_blade_center * _rel_blade_center /(0.5*0.5);
float speed=_rotor_rpm/60*_diameter*_rel_blade_center*pi; float speed=_rotor_rpm/60*_diameter*_rel_blade_center*pi;
float lentocenter=_diameter*_rel_blade_center*0.5; float lentocenter=_diameter*_rel_blade_center*0.5;
float lentoforceattac=_diameter*_rel_len_hinge*0.5; // float lentoforceattac=_diameter*_rel_len_hinge*0.5;
float zentforce=rotorpartmass*speed*speed/lentocenter; float zentforce=rotorpartmass*speed*speed/lentocenter;
float pitchaforce=_force_at_pitch_a/_number_of_parts*.453*9.81; float pitchaforce=_force_at_pitch_a/_number_of_parts*.453*9.81;
// was pounds of force, now N, devided by _number_of_parts // was pounds of force, now N, devided by _number_of_parts
@ -1196,8 +1196,8 @@ void Rotor::compile()
float relamp=(omega*omega/(2*_delta*Math::sqrt(sqr(omega0*omega0-omega*omega) float relamp=(omega*omega/(2*_delta*Math::sqrt(sqr(omega0*omega0-omega*omega)
+4*_delta*_delta*omega*omega)))*_cyclic_factor; +4*_delta*_delta*omega*omega)))*_cyclic_factor;
float relamp_theoretical=(omega*omega/(2*delta_theoretical*Math::sqrt(sqr(omega0*omega0-omega*omega) //float relamp_theoretical=(omega*omega/(2*delta_theoretical*Math::sqrt(sqr(omega0*omega0-omega*omega)
+4*delta_theoretical*delta_theoretical*omega*omega)))*_cyclic_factor; // +4*delta_theoretical*delta_theoretical*omega*omega)))*_cyclic_factor;
_phi=Math::acos(_rel_len_hinge); _phi=Math::acos(_rel_len_hinge);
_phi-=Math::atan(_delta3); _phi-=Math::atan(_delta3);
if (!_no_torque) if (!_no_torque)
@ -1528,7 +1528,7 @@ void Rotorgear::calcForces(float* torqueOut)
total_torque+=r->getTorque()*omegan; total_torque+=r->getTorque()*omegan;
} }
float max_torque_of_engine=0; float max_torque_of_engine=0;
SGPropertyNode * node=fgGetNode("/rotors/gear", true); // SGPropertyNode * node=fgGetNode("/rotors/gear", true);
if (_engineon) if (_engineon)
{ {
max_torque_of_engine=_max_power_engine*_max_rel_torque; max_torque_of_engine=_max_power_engine*_max_rel_torque;
@ -1599,7 +1599,7 @@ void Rotorgear::calcForces(float* torqueOut)
for(j=0; j<_rotors.size(); j++) { for(j=0; j<_rotors.size(); j++) {
Rotor* r = (Rotor*)_rotors.get(j); Rotor* r = (Rotor*)_rotors.get(j);
for(i=0; i<r->_rotorparts.size(); i++) { for(i=0; i<r->_rotorparts.size(); i++) {
float torque_scalar=0; // float torque_scalar=0;
Rotorpart* rp = (Rotorpart*)r->_rotorparts.get(i); Rotorpart* rp = (Rotorpart*)r->_rotorparts.get(i);
float torque[3]; float torque[3];
rp->getAccelTorque(_ddt_omegarel,torque); rp->getAccelTorque(_ddt_omegarel,torque);
@ -1619,7 +1619,7 @@ void Rotorgear::addRotor(Rotor* rotor)
void Rotorgear::compile() void Rotorgear::compile()
{ {
float wgt = 0; // float wgt = 0;
for(int j=0; j<_rotors.size(); j++) { for(int j=0; j<_rotors.size(); j++) {
Rotor* r = (Rotor*)_rotors.get(j); Rotor* r = (Rotor*)_rotors.get(j);
r->compile(); r->compile();

10
src/FDM/YASim/yasim-test.cpp
View file

@ -35,11 +35,11 @@ static const float KTS2MPS = 0.514444444444;
// numbers: "aoa lift drag LD" (aoa in degrees, lift and drag in // numbers: "aoa lift drag LD" (aoa in degrees, lift and drag in
// G's). You can use this in gnuplot like so (assuming the output is // G's). You can use this in gnuplot like so (assuming the output is
// in a file named "dat": // in a file named "dat":
// /*
// plot "dat" using 1:2 with lines title 'lift', \ plot "dat" using 1:2 with lines title 'lift', \
// "dat" using 1:3 with lines title 'drag', \ "dat" using 1:3 with lines title 'drag', \
// "dat" using 1:4 with lines title 'LD' "dat" using 1:4 with lines title 'LD'
// */
void yasim_graph(Airplane* a, float alt, float kts) void yasim_graph(Airplane* a, float alt, float kts)
{ {
Model* m = a->getModel(); Model* m = a->getModel();