From e32491d749cdaab21e24e4084963edc486b468fb Mon Sep 17 00:00:00 2001 From: Jason Short Date: Sun, 11 Nov 2012 18:17:33 -0800 Subject: [PATCH] ACM: Added a speed filter for throttle cruise, increased alt change rate for alt hold, increased the max climb_rate reporting --- ArduCopter/ArduCopter.pde | 8 ++++---- 1 file changed, 4 insertions(+), 4 deletions(-) diff --git a/ArduCopter/ArduCopter.pde b/ArduCopter/ArduCopter.pde index d91593a887..27216bf19a 100644 --- a/ArduCopter/ArduCopter.pde +++ b/ArduCopter/ArduCopter.pde @@ -1723,7 +1723,7 @@ void update_throttle_mode(void) throttle_avg = g.throttle_cruise; } // calc average throttle - if ((g.rc_3.control_in > g.throttle_min) && abs(climb_rate) < 60) { + if ((g.rc_3.control_in > g.throttle_min) && (abs(climb_rate) < 60) && (g_gps->ground_speed < 200)) { throttle_avg = throttle_avg * .99 + (float)g.rc_3.control_in * .01; g.throttle_cruise = throttle_avg; } @@ -1748,13 +1748,13 @@ void update_throttle_mode(void) case THROTTLE_HOLD: // allow interactive changing of atitude if(g.rc_3.radio_in < (g.rc_3.radio_min + 200)){ - int16_t _rate = 120 - (((g.rc_3.radio_in - g.rc_3.radio_min) * 12) / 20); + int16_t _rate = 180 - (((g.rc_3.radio_in - g.rc_3.radio_min) * 12) / 20); reset_throttle_counter = 150; nav_throttle = get_throttle_rate(-_rate); g.rc_3.servo_out = g.throttle_cruise + nav_throttle + angle_boost; break; }else if(g.rc_3.radio_in > (g.rc_3.radio_max - 200)){ - int16_t _rate = 180 - ((g.rc_3.radio_max - g.rc_3.radio_in) * 18) / 20; + int16_t _rate = 300 - ((g.rc_3.radio_max - g.rc_3.radio_in) * 18) / 20; reset_throttle_counter = 150; nav_throttle = get_throttle_rate(_rate); g.rc_3.servo_out = g.throttle_cruise + nav_throttle + angle_boost; @@ -1885,7 +1885,7 @@ static void update_altitude() // 2.6 way int16_t temp = (baro_alt - old_baro_alt) * 10; baro_rate = (temp + baro_rate) >> 1; - baro_rate = constrain(baro_rate, -300, 300); + baro_rate = constrain(baro_rate, -500, 500); old_baro_alt = baro_alt; // Using Tridge's new clamb rate calc