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Arducopter: Toy mode refinements

This commit is contained in:
Jason Short 2012-07-10 21:45:25 -07:00
parent 1bd1975e2e
commit 23f8d20271
1 changed files with 15 additions and 8 deletions
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23
ArduCopter/Attitude.pde
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@ -707,17 +707,18 @@ void roll_pitch_toy()
// Yaw control - Yaw is always available, and will NOT exit the
// user from Loiter mode
int16_t yaw_rate = g.rc_1.control_in / g.toy_yaw_rate;
int16_t yaw_rate = g.rc_1.control_in;// / g.toy_yaw_rate;
//nav_yaw += yaw_rate / 100;
//nav_yaw = wrap_360(nav_yaw);
//g.rc_4.servo_out = get_stabilize_yaw(nav_yaw);
if(g.rc_1.control_in != 0){
g.rc_4.servo_out = get_rate_yaw(yaw_rate);
if(g.rc_1.control_in != 0){ // roll
g.rc_4.servo_out = get_acro_yaw(yaw_rate);
yaw_stopped = false;
yaw_timer = 150;
}else if (!yaw_stopped){
g.rc_4.servo_out = get_rate_yaw(0);
g.rc_4.servo_out = get_acro_yaw(0);
yaw_timer--;
if(yaw_timer == 0){
yaw_stopped = true;
@ -728,7 +729,6 @@ void roll_pitch_toy()
g.rc_4.servo_out = get_stabilize_yaw(nav_yaw);
}
if(manual_control){
// user is in control: reset count-up timer
toy_input_timer = 0;
@ -761,14 +761,21 @@ void roll_pitch_toy()
else if(yaw_rate < 0)
roll_rate = -roll_rate;
roll_rate = constrain(roll_rate, -(4500 / g.toy_yaw_rate.get()), (4500 / g.toy_yaw_rate.get()));
int16_t roll_limit = 4500 / g.toy_yaw_rate;
roll_rate = constrain(roll_rate, -roll_limit, roll_limit);
#else
// yaw_rate = roll angle
// Linear equation for Yaw:Speed to Roll
// default is 1000, lower for more roll action
roll_rate = (g_gps->ground_speed / 1000) * yaw_rate;
//roll_rate = ((float)g_gps->ground_speed / 600) * (float)yaw_rate;
roll_rate = ((int32_t)g.rc_2.control_in * (yaw_rate/100)) /20;
Serial.printf("roll_rate: %d\n",roll_rate);
// limit roll rate to 15, 30, or 45 deg per second.
roll_rate = constrain(roll_rate, -(4500 / g.toy_yaw_rate.get()), (4500 / g.toy_yaw_rate.get()));
int16_t roll_limit = 4500 / g.toy_yaw_rate;
roll_rate = constrain(roll_rate, -roll_limit, roll_limit);
Serial.printf("yaw_rate %d, roll_rate %d, lim %d\n",yaw_rate, roll_rate, roll_limit);
#endif
// Output the attitude