fly/flightgear
1
0
Fork 0
Code Activity

Added support for rotational rates and body access (pilot relative)

Browse source 
accelerations.
This commit is contained in:
curt 2002-03-27 05:21:38 +00:00
parent 2e34bfc5af
commit ca364c2cd9
1 changed files with 20 additions and 2 deletions
Show stats Download patch file Download diff file Expand all files Collapse all files

22
src/FDM/ExternalNet.cxx
View file

@ -65,6 +65,8 @@ static void htond (double &x)
static void global2raw( FGRawCtrls *raw ) {
int i;
#if 0
// these can probably get wiped as soon as David spots them. :-)
static const SGPropertyNode *aileron
= fgGetNode("/controls/aileron");
static const SGPropertyNode *elevator
@ -75,6 +77,8 @@ static void global2raw( FGRawCtrls *raw ) {
= fgGetNode("/controls/rudder");
static const SGPropertyNode *flaps
= fgGetNode("/controls/flaps");
#endif
char buf[256];
// fill in values
@ -97,6 +101,8 @@ static void global2raw( FGRawCtrls *raw ) {
raw->brake[i] = fgGetDouble( buf );
}
raw->hground = fgGetDouble( "/environment/ground-elevation-m" );
raw->magvar = fgGetDouble("/environment/magnetic-variation-deg");
raw->speedup = fgGetInt("/sim/speed-up");
// convert to network byte order
raw->version = htonl(raw->version);
@ -114,7 +120,8 @@ static void global2raw( FGRawCtrls *raw ) {
htond(raw->brake[i]);
}
htond(raw->hground);
htond(raw->magvar);
raw->speedup = htonl(raw->speedup);
}
@ -127,8 +134,14 @@ static void net2global( FGNetFDM *net ) {
htond(net->phi);
htond(net->theta);
htond(net->psi);
htond(net->phidot);
htond(net->thetadot);
htond(net->psidot);
htond(net->vcas);
htond(net->climb_rate);
htond(net->A_X_pilot);
htond(net->A_Y_pilot);
htond(net->A_Z_pilot);
net->cur_time = ntohl(net->cur_time);
net->warp = ntohl(net->warp);
htond(net->visibility);
@ -143,9 +156,14 @@ static void net2global( FGNetFDM *net ) {
cur_fdm_state->_set_Euler_Angles( net->phi,
net->theta,
net->psi );
cur_fdm_state->_set_Euler_Rates( net->phidot,
net->thetadot,
net->psidot );
cur_fdm_state->_set_V_calibrated_kts( net->vcas );
cur_fdm_state->_set_Climb_Rate( net->climb_rate );
cur_fdm_state->_set_Accels_Pilot_Body( net->A_X_pilot,
net->A_Y_pilot,
net->A_Z_pilot );
/* these are ignored for now ... */
/*
if ( net->cur_time ) {