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Fix error with calc_nav_pitch_roll

This commit is contained in:
Jason Short 2011-11-28 21:26:55 -08:00
parent b3b218fa40
commit 7e1d41be14
1 changed files with 1 additions and 4 deletions
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5
ArduCopter/navigation.pde
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@ -169,7 +169,6 @@ static void calc_nav_rate(int max_speed)
max_speed = min(max_speed, waypoint_speed_gov);
}
// XXX target_angle should be the original desired target angle!
//float temp = radians((target_bearing - g_gps->ground_course)/100.0);
float temp = (target_bearing - g_gps->ground_course) * RADX100;
@ -187,8 +186,6 @@ static void calc_nav_rate(int max_speed)
y_rate_error = max_speed - y_actual_speed; // 413
y_rate_error = constrain(y_rate_error, -800, 800); // added a rate error limit to keep pitching down to a minimum
nav_lat = constrain(g.pi_nav_lat.get_pi(y_rate_error, dTnav), -3500, 3500);
// 400cm/s * 3 = 1200 or 12 deg pitch
// 800cm/s * 3 = 2400 or 24 deg pitch MAX
// nav_lat and nav_lon will be rotated to the angle of the quad in calc_nav_pitch_roll()
@ -227,7 +224,7 @@ static int32_t cross_track_test()
// nav_roll, nav_pitch
static void calc_nav_pitch_roll()
{
float temp = (9000l - (dcm.yaw_sensor - original_target_bearing)) * RADX100;
float temp = (9000l - (dcm.yaw_sensor - target_bearing)) * RADX100;
//t: 1.5465, t1: -10.9451, t2: 1.5359, t3: 1.5465
float _cos_yaw_x = cos(temp);