]> git.mxchange.org Git - flightgear.git/commitdiff
Tweaks to autopilot, but I'm not 100% happy with the current state of things.
authorcurt <curt>
Fri, 26 Jan 2001 00:20:18 +0000 (00:20 +0000)
committercurt <curt>
Fri, 26 Jan 2001 00:20:18 +0000 (00:20 +0000)
src/Autopilot/newauto.cxx

index 196791aefae910a8f077af0ef3a24867cbad97c3..b021a786097717fb9ce0dffc5b30ece563cc8b7b 100644 (file)
@@ -107,6 +107,14 @@ static inline double get_ground_speed() {
 
 
 void FGAutopilot::MakeTargetWPStr( double distance ) {
+    static time_t last_time = 0;
+    time_t current_time = time(NULL);
+    if ( last_time == current_time ) {
+       return;
+    }
+
+    last_time = current_time;
+
     double accum = 0.0;
 
     int size = globals->get_route()->size();
@@ -529,10 +537,28 @@ int FGAutopilot::run() {
            double x = current_radiostack->get_nav1_gs_dist();
            double y = (FGBFI::getAltitude() 
                        - current_radiostack->get_nav1_elev()) * FEET_TO_METER;
-           double angle = atan2( y, x ) * RAD_TO_DEG;
-           double gs_diff = current_radiostack->get_nav1_target_gs() - angle;
-           climb_error_accum += gs_diff * 2.0;
-           TargetClimbRate = gs_diff * 200.0 + climb_error_accum;
+           double current_angle = atan2( y, x ) * RAD_TO_DEG;
+           // cout << "current angle = " << current_angle << endl;
+
+           double target_angle = current_radiostack->get_nav1_target_gs();
+           // cout << "target angle = " << target_angle << endl;
+
+           double gs_diff = target_angle - current_angle;
+           // cout << "difference from desired = " << gs_diff << endl;
+
+           // convert desired vertical path angle into a climb rate
+           double des_angle = current_angle - 10 * gs_diff;
+           // cout << "desired angle = " << des_angle << endl;
+
+           // convert to meter/min
+           // cout << "raw ground speed = " << cur_fdm_state->get_V_ground_speed() << endl;
+           double horiz_vel = cur_fdm_state->get_V_ground_speed()
+               * FEET_TO_METER * 60.0;
+           // cout << "Horizontal vel = " << horiz_vel << endl;
+           TargetClimbRate = -sin( des_angle * DEG_TO_RAD ) * horiz_vel;
+           // cout << "TargetClimbRate = " << TargetClimbRate << endl;
+           /* climb_error_accum += gs_diff * 2.0; */
+           /* TargetClimbRate = gs_diff * 200.0 + climb_error_accum; */
        } else if ( altitude_mode == FG_ALTITUDE_TERRAIN ) {
            // brain dead ground hugging with no look ahead
            TargetClimbRate =
@@ -584,7 +610,7 @@ int FGAutopilot::run() {
        // calculate integral error, and adjustment amount
        int_error = alt_error_accum;
        // printf("error = %.2f  int_error = %.2f\n", error, int_error);
-       int_adj = int_error / 8000.0;
+       int_adj = int_error / 20000.0;
 
        // caclulate proportional error
        prop_error = error;