int parseAxis(const char* name);
int parseOutput(const char* name);
void parseWeight(XMLAttributes* a);
+ void parseTurbineEngine(XMLAttributes* a);
+ void parsePistonEngine(XMLAttributes* a);
void parsePropeller(XMLAttributes* a);
bool eq(const char* a, const char* b);
+ bool caseeq(const char* a, const char* b);
char* dup(const char* s);
int attri(XMLAttributes* atts, char* attr);
int attri(XMLAttributes* atts, char* attr, int def);
float attrf(XMLAttributes* atts, char* attr);
float attrf(XMLAttributes* atts, char* attr, float def);
- bool attristrue(XMLAttributes* atts, char* attr);
+ bool attrb(XMLAttributes* atts, char* attr);
// The core Airplane object we manage.
Airplane _airplane;
+ // Aerodynamic turbulence model
+ Turbulence* _turb;
+
// The list of "axes" that we expect to find as input. These are
// typically property names.
Vector _axes;