removed D for nav, added extra timer for FBW and Nav.
git-svn-id: https://arducopter.googlecode.com/svn/trunk@1600 f9c3cf11-9bcb-44bc-f272-b75c42450872
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@ -388,11 +388,13 @@ byte slow_loopCounter;
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byte superslow_loopCounter;
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byte superslow_loopCounter;
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unsigned long nav_loopTimer; // used to track the elapsed ime for GPS nav
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unsigned long nav_loopTimer; // used to track the elapsed ime for GPS nav
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unsigned long nav2_loopTimer; // used to track the elapsed ime for GPS nav
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uint8_t delta_ms_medium_loop;
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uint8_t delta_ms_medium_loop;
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uint8_t delta_ms_fast_loop; // Delta Time in miliseconds
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uint8_t delta_ms_fast_loop; // Delta Time in miliseconds
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unsigned long dTnav; // Delta Time in milliseconds for navigation computations
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unsigned long dTnav; // Delta Time in milliseconds for navigation computations
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unsigned long dTnav2; // Delta Time in milliseconds for navigation computations
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unsigned long elapsedTime; // for doing custom events
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unsigned long elapsedTime; // for doing custom events
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float load; // % MCU cycles used
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float load; // % MCU cycles used
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@ -535,6 +537,8 @@ void medium_loop()
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// calc pitch and roll to target
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// calc pitch and roll to target
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// -----------------------------
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// -----------------------------
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dTnav2 = millis() - nav2_loopTimer;
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nav2_loopTimer = millis();
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calc_nav();
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calc_nav();
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break;
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break;
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@ -860,6 +864,7 @@ void update_current_flight_mode(void)
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fbw_timer = 0;
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fbw_timer = 0;
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if(home_is_set == false){
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if(home_is_set == false){
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scaleLongDown = 1;
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// we are not using GPS
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// we are not using GPS
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// reset the location
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// reset the location
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// RTL won't function
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// RTL won't function
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@ -869,8 +874,8 @@ void update_current_flight_mode(void)
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dTnav = 200;
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dTnav = 200;
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}
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}
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next_WP.lat = home.lat + rc_2.control_in / 5; // 4500 / 5 = 900 = 10 meteres
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next_WP.lat = home.lat + rc_2.control_in / 2; // 4500 / 2 = 2250 = 25 meteres
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next_WP.lng = home.lng + rc_1.control_in / 5; // 4500 / 5 = 900 = 10 meteres
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next_WP.lng = home.lng + rc_1.control_in / 2; // 4500 / 2 = 900 = 25 meteres
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}
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}
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// Output Pitch, Roll, Yaw and Throttle
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// Output Pitch, Roll, Yaw and Throttle
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@ -1013,4 +1018,6 @@ void read_AHRS(void)
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//-----------------------------------------------
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//-----------------------------------------------
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dcm.update_DCM(G_Dt);
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dcm.update_DCM(G_Dt);
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omega = dcm.get_gyro();
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omega = dcm.get_gyro();
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dcm.roll_sensor = 0;
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dcm.pitch_sensor = 0;
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}
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}
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@ -355,7 +355,7 @@
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//
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//
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// how much to we pitch towards the target
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// how much to we pitch towards the target
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#ifndef PITCH_MAX
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#ifndef PITCH_MAX
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# define PITCH_MAX 21
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# define PITCH_MAX 25
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#endif
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#endif
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@ -363,13 +363,13 @@
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// Navigation control gains
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// Navigation control gains
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//
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//
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#ifndef NAV_P
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#ifndef NAV_P
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# define NAV_P 2.4
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# define NAV_P 1.5
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#endif
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#endif
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#ifndef NAV_I
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#ifndef NAV_I
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# define NAV_I 0.01
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# define NAV_I 0.00
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#endif
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#endif
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#ifndef NAV_D
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#ifndef NAV_D
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# define NAV_D 0.005
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# define NAV_D 0.00
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#endif
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#endif
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#ifndef NAV_IMAX
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#ifndef NAV_IMAX
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# define NAV_IMAX 250
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# define NAV_IMAX 250
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@ -386,7 +386,7 @@
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# define THROTTLE_BARO_I 0.04
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# define THROTTLE_BARO_I 0.04
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#endif
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#endif
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#ifndef THROTTLE_BARO_D
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#ifndef THROTTLE_BARO_D
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# define THROTTLE_BARO_D 0.15
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# define THROTTLE_BARO_D 0.45
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#endif
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#endif
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#ifndef THROTTLE_BARO_IMAX
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#ifndef THROTTLE_BARO_IMAX
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# define THROTTLE_BARO_IMAX 100
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# define THROTTLE_BARO_IMAX 100
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