mirror of
https://github.com/paparazzi/paparazzi.git
synced 2026-06-02 13:27:32 +08:00
airspeed max throttle - visualtarget/opticflow/energyctrl messages
This commit is contained in:
+35
-6
@@ -322,6 +322,15 @@
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<field name="groundspeed_sp" type="float" unit="m/s"/>
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<field name="groundspeed_sp" type="float" unit="m/s"/>
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</message>
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</message>
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<message name="AIRSPEED" id="54">
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<field name="adc" type="uint16"/>
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<field name="airspeed" type="float" unit="m/s"/>
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<field name="airspeed_sp" type="float" unit="m/s"/>
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<field name="airspeed_cnt" type="float" unit="m/s"/>
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<field name="groundspeed_sp" type="float" unit="m/s"/>
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</message>
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<message name="BARO_WORDS" id="46">
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<message name="BARO_WORDS" id="46">
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<field name="w1" type="uint16"/>
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<field name="w1" type="uint16"/>
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<field name="w2" type="uint16"/>
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<field name="w2" type="uint16"/>
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@@ -366,6 +375,11 @@
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<field name="values" type="int16[]" alt_unit_coef="1e-3"/>
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<field name="values" type="int16[]" alt_unit_coef="1e-3"/>
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</message>
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</message>
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<message name="VISUALTARGET" id="235">
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<field name="x" type="uint16"></field>
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<field name="y" type="uint16"></field>
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</message>
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<message name="DEBUG_IR_I2C" id="53">
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<message name="DEBUG_IR_I2C" id="53">
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<field name="top" type="int16" unit="adc"></field>
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<field name="top" type="int16" unit="adc"></field>
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</message>
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</message>
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@@ -526,6 +540,11 @@
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<field name="values" type="uint16[]" unit="ticks"/>
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<field name="values" type="uint16[]" unit="ticks"/>
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</message>
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</message>
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<message name="OPTICFLOW" id="234">
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<field name="flow" type="uint16"></field>
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<field name="ref_alt" type="float"></field>
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</message>
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<message name="RC" id="101">
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<message name="RC" id="101">
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<field name="values" type="int16[]" unit="pprz" format="%d"/>
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<field name="values" type="int16[]" unit="pprz" format="%d"/>
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</message>
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</message>
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@@ -550,12 +569,12 @@
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<field name="values" type="uint16[]" unit="none"/>
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<field name="values" type="uint16[]" unit="none"/>
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</message>
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</message>
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<message name="BETH" id="106">
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<message name="BETH" id="106">
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<field name="azimuth" type="uint16"/>
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<field name="azimuth" type="uint16"/>
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<field name="elevation" type="uint16"/>
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<field name="elevation" type="uint16"/>
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<field name="tilt" type="uint16"/>
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<field name="tilt" type="uint16"/>
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<field name="other" type="uint16"/>
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<field name="other" type="uint16"/>
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</message>
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</message>
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<message name="DC_SHOT" id="110">
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<message name="DC_SHOT" id="110">
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<field name="photo_nr" type="int16" unit=""></field>
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<field name="photo_nr" type="int16" unit=""></field>
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@@ -597,6 +616,16 @@
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<field name="climb" type="float"/>
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<field name="climb" type="float"/>
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</message>
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</message>
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<message name="VERTICAL_ENERGY" id="124">
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<field name="Epot_err" type="float"/>
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<field name="Ekin_err" type="float"/>
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<field name="Etot_err" type="float"/>
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<field name="Edis_err" type="float"/>
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<field name="throttle" type="float"/>
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<field name="nav_pitch" type="float"/>
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<field name="speed_sp" type="float"/>
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</message>
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<message name="BOOZ2_STAB_ATTITUDE_FLOAT" id="130">
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<message name="BOOZ2_STAB_ATTITUDE_FLOAT" id="130">
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<field name="est_p" type="float" alt_unit="degres/s" alt_unit_coef="57.29578"/>
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<field name="est_p" type="float" alt_unit="degres/s" alt_unit_coef="57.29578"/>
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<field name="est_q" type="float" alt_unit="degres/s" alt_unit_coef="57.29578"/>
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<field name="est_q" type="float" alt_unit="degres/s" alt_unit_coef="57.29578"/>
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@@ -205,4 +205,24 @@
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</class>
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</class>
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<class name="MAVPILOT" ID="100">
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<message name="COMMAND" ID="0x05" length="12">
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<field name="S1" format="U2"/>
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<field name="S2" format="U2"/>
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<field name="S3" format="U2"/>
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<field name="S4" format="U2"/>
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<field name="S5" format="U2"/>
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<field name="S6" format="U2"/>
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</message>
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<message name="FBW" ID="0x06" length="6">
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<field name="MOD" format="U1"/>
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<field name="STAT" format="U1"/>
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<field name="ERR" format="U1"/>
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<field name="VOLT" format="U1"/>
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<field name="CURRENT" format="U2" />
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</message>
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</class>
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</ubx>
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</ubx>
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@@ -336,6 +336,7 @@ inline static void v_ctl_climb_auto_throttle_loop(void) {
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controlled_throttle = (err_airspeed + v_ctl_auto_airspeed_sum_err * v_ctl_auto_airspeed_igain) * v_ctl_auto_airspeed_pgain;
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controlled_throttle = (err_airspeed + v_ctl_auto_airspeed_sum_err * v_ctl_auto_airspeed_igain) * v_ctl_auto_airspeed_pgain;
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// Done, set outputs
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// Done, set outputs
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Bound(controlled_throttle, 0, V_CTL_AUTO_THROTTLE_MAX_CRUISE_THROTTLE);
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f_throttle = controlled_throttle;
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f_throttle = controlled_throttle;
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nav_pitch = v_ctl_pitch_of_vz;
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nav_pitch = v_ctl_pitch_of_vz;
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v_ctl_throttle_setpoint = TRIM_UPPRZ(f_throttle * MAX_PPRZ);
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v_ctl_throttle_setpoint = TRIM_UPPRZ(f_throttle * MAX_PPRZ);
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@@ -69,7 +69,7 @@
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#include "adc_generic.h"
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#include "adc_generic.h"
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#endif
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#endif
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#ifdef USE_AIRSPEED
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#if defined USE_AIRSPEED || defined MEASURE_AIRSPEED
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#include "airspeed.h"
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#include "airspeed.h"
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#endif
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#endif
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@@ -147,9 +147,6 @@
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#include "osam_imu_ugear.h"
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#include "osam_imu_ugear.h"
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#endif
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#endif
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#ifdef XSENS
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#include "xsens_ins.h"
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#endif
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/*code added by Haiyang Chao ends*/
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/*code added by Haiyang Chao ends*/
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#if ! defined CATASTROPHIC_BAT_LEVEL && defined LOW_BATTERY
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#if ! defined CATASTROPHIC_BAT_LEVEL && defined LOW_BATTERY
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@@ -659,7 +656,8 @@ void periodic_task_ap( void ) {
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#if defined GYRO
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#if defined GYRO
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gyro_update();
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gyro_update();
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#endif
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#endif
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#if defined USE_AIRSPEED
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#if defined USE_AIRSPEED || defined MEASURE_AIRSPEED
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airspeed_update();
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airspeed_update();
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#endif
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#endif
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#ifdef INFRARED
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#ifdef INFRARED
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@@ -711,7 +709,7 @@ void init_ap( void ) {
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#ifdef GYRO
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#ifdef GYRO
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gyro_init();
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gyro_init();
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#endif
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#endif
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#ifdef USE_AIRSPEED
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#if defined USE_AIRSPEED || defined MEASURE_AIRSPEED
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airspeed_init();
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airspeed_init();
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#endif
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#endif
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#ifdef GPS
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#ifdef GPS
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@@ -913,6 +911,9 @@ void event_task_ap( void ) {
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gps_verbose_downlink = !launch;
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gps_verbose_downlink = !launch;
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UseGpsPosNoSend(estimator_update_state_gps);
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UseGpsPosNoSend(estimator_update_state_gps);
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gps_downlink();
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gps_downlink();
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#ifdef GPS_TRIGGERED_FUNCTION
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GPS_TRIGGERED_FUNCTION();
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#endif
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gps_pos_available = FALSE;
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gps_pos_available = FALSE;
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}
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}
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}
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}
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