Added Iris airframe and 3dr radio

This commit is contained in:
kevindehecker
2016-03-04 15:26:04 +01:00
parent 0ec787c365
commit 03dd41f641
7 changed files with 565 additions and 1 deletions
+11
View File
@@ -109,6 +109,17 @@
settings_modules="modules/gps_ubx_ucenter.xml modules/logger_sd_spi_direct.xml"
gui_color="#9b69e5ce9e7a"
/>
<aircraft
name="Iris"
ac_id="66"
airframe="airframes/TUDELFT/tudelft_iris_indi.xml"
radio="radios/FrSky3dr.xml"
telemetry="telemetry/default_rotorcraft_slow.xml"
flight_plan="flight_plans/TUDELFT/tudelft_delft_basic.xml"
settings="settings/rotorcraft_basic.xml settings/control/rotorcraft_guidance.xml [settings/control/stabilization_att_int_quat.xml] settings/control/stabilization_indi.xml"
settings_modules="modules/geo_mag.xml modules/air_data.xml modules/gps_ubx_ucenter.xml"
gui_color="#ffffcccaccca"
/>
<aircraft
name="Logo600"
ac_id="111"
@@ -89,6 +89,16 @@
<arg flag="-speech" />
</program>
</session>
<session name="Flight Paparazzi @57600">
<program name="Data Link">
<arg flag="-d" constant="/dev/paparazzi/link"/>
<arg flag="-s" constant="57600"/>
</program>
<program name="Server"/>
<program name="GCS">
<arg flag="-speech" />
</program>
</session>
<session name="Flight ACM1 @57600">
<program name="Data Link">
<arg flag="-d" constant="/dev/ttyACM1"/>
@@ -0,0 +1,250 @@
<!DOCTYPE airframe SYSTEM "../airframe.dtd">
<?xml version="1.0" encoding="UTF-8"?>
<!-- this is a quadrotor frame equiped with
* Autopilot: 3dr Pixhawk 2.4
* IMU: MPU6000 + L3GD20 + LSM303D
* Actuators: PWM motor controllers?
* GPS: Ublox http://wiki.paparazziuav.org/wiki/Subsystem/gps
* RC: PPM
-->
<airframe name="iris_indi">
<firmware name="rotorcraft">
<target name="ap" board="px4fmu_2.4" />
<define name="BAT_CHECKER_DELAY" value="80" />
<!-- amount of time it take for the bat to check -->
<!-- to avoid bat low spike detection when strong pullup withch draws short sudden power-->
<define name="CATASTROPHIC_BATTERY_KILL_DELAY" value="80" />
<!-- in seconds-->
<target name="nps" board="pc">
<subsystem name="fdm" type="jsbsim" />
<subsystem name="udp" />
</target>
<subsystem name="telemetry" type="transparent" />
<!-- <subsystem name="imu" type="px4fmu_v2.4">-->
<subsystem name="imu" type="mpu6000">
<configure name="IMU_MPU_SPI_DEV" value="spi1" />
<configure name="IMU_MPU_SPI_SLAVE_IDX" value="SPI_SLAVE2" />
</subsystem>
<subsystem name="gps" type="ublox" />
<subsystem name="stabilization" type="indi" />
<subsystem name="ahrs" type="int_cmpl_quat" />
<subsystem name="ins" type="extended" />
<subsystem name="current_sensor">
<configure name="ADC_CURRENT_SENSOR" value="ADC_3" />
</subsystem>
<subsystem name="intermcu" type="uart">
<configure name="INTERMCU_PORT" value="UART6" />
<configure name="INTERMCU_BAUD" value="B1500000" />
</subsystem>
</firmware>
<firmware name="rotorcraft">
<target name="fbw" board="px4io_2.4" />
<subsystem name="motor_mixing" />
<subsystem name="radio_control" type="ppm">
<define name="USE_KILL_SWITCH_FOR_MOTOR_ARMING" value="1" />
<define name="RADIO_KILL_SWITCH" value="RADIO_KILL" />
</subsystem>
<!-- <subsystem name="radio_control" type="spektrum">-->
<!-- <define name="RADIO_CONTROL_SPEKTRUM_NO_SIGN" value="1"/>-->
<!-- <define name="USE_KILL_SWITCH_FOR_MOTOR_ARMING" value="1"/>-->
<!-- <define name="RADIO_FBW_MODE" value="RADIO_AUX2"/>-->
<!-- <define name="RADIO_MODE" value="RADIO_GEAR"/>-->
<!-- <define name="SPEKTRUM_HAS_SOFT_BIND_PIN" value="1"/>-->
<!-- </subsystem>-->
<subsystem name="actuators" type="pwm">
<define name="SERVO_HZ" value="400" />
</subsystem>
<define name="RC_LOST_FBW_MODE" value="FBW_MODE_FAILSAFE" />
<!-- Switch to Failsafe or to Autopilot on RC loss? -->
<define name="RC_LOST_IN_AUTO_FBW_MODE" value="FBW_MODE_AUTO" />
<define name="AP_LOST_FBW_MODE" value="FBW_MODE_MANUAL" />
<!-- Switch to Failsafe or to Manual on AP loss? -->
<define name="INTERMCU_LOST_CNT" value="100" />
<subsystem name="intermcu" type="uart">
<configure name="INTERMCU_PORT" value="UART2" />
<configure name="INTERMCU_BAUD" value="B1500000" />
</subsystem>
</firmware>
<firmware name="test_progs">
<target name="test_telemetry" board="px4fmu_2.4" />
</firmware>
<firmware name="test_progs">
<target name="test_baro_board" board="px4fmu_2.4" />
</firmware>
<firmware name="test_progs">
<target name="test_datalink" board="px4fmu_2.4" />
</firmware>
<modules main_freq="512">
<load name="px4io_flash.xml" />
<load name="geo_mag.xml" />
<load name="air_data.xml" />
<load name="send_imu_mag_current.xml" />
<load name="gps_ubx_ucenter.xml" />
<!-- <load name="spektrum_soft_bind.xml"/>-->
</modules>
<section name="MISC">
<define name="MilliAmpereOfAdc(adc)" value="((float)adc) * (3.3f / 4096.0f) * (90.0f / 5.0f)" />
<!-- 100Amp = 2Volt -> 2482,42 tick/100Amp"(0.0402832*adc)" -->
</section>
<section name="IMU" prefix="IMU_">
<!-- replace this with your own calibration -->
<define name="MAG_X_NEUTRAL" value="14" />
<define name="MAG_Y_NEUTRAL" value="116" />
<define name="MAG_Z_NEUTRAL" value="119" />
<define name="MAG_X_SENS" value="5.09245681612" integer="16" />
<define name="MAG_Y_SENS" value="5.29702744632" integer="16" />
<define name="MAG_Z_SENS" value="5.65287938992" integer="16" />
<define name="BODY_TO_IMU_PHI" value="180." unit="deg" />
<define name="BODY_TO_IMU_THETA" value="180." unit="deg" />
<define name="BODY_TO_IMU_PSI" value="90." unit="deg" />
</section>
<commands>
<axis name="PITCH" failsafe_value="0" />
<axis name="ROLL" failsafe_value="0" />
<axis name="YAW" failsafe_value="0" />
<axis name="THRUST" failsafe_value="0" />
</commands>
<rc_commands>
<set command="THRUST" value="@THROTTLE" />
<set command="ROLL" value="@ROLL" />
<set command="PITCH" value="@PITCH" />
<set command="YAW" value="@YAW" />
</rc_commands>
<servos driver="Default">
<servo name="TOP_LEFT" no="2" min="1140" neutral="1280" max="1850" />
<servo name="TOP_RIGHT" no="0" min="1140" neutral="1280" max="1850" />
<servo name="BOTTOM_RIGHT" no="3" min="1140" neutral="1280" max="1850" />
<servo name="BOTTOM_LEFT" no="1" min="1140" neutral="1280" max="1850" />
</servos>
<section name="MIXING" prefix="MOTOR_MIXING_">
<define name="TRIM_ROLL" value="0" />
<define name="TRIM_PITCH" value="0" />
<define name="TRIM_YAW" value="0" />
<define name="REVERSE" value="FALSE" />
<define name="TYPE" value="QUAD_X" />
</section>
<command_laws>
<call fun="motor_mixing_run(autopilot_motors_on,FALSE,values)" />
<set servo="TOP_LEFT" value="motor_mixing.commands[MOTOR_FRONT_LEFT]" />
<set servo="TOP_RIGHT" value="motor_mixing.commands[MOTOR_FRONT_RIGHT]" />
<set servo="BOTTOM_RIGHT" value="motor_mixing.commands[MOTOR_BACK_RIGHT]" />
<set servo="BOTTOM_LEFT" value="motor_mixing.commands[MOTOR_BACK_LEFT]" />
</command_laws>
<section name="AIR_DATA" prefix="AIR_DATA_">
<define name="CALC_AIRSPEED" value="FALSE" />
<define name="CALC_TAS_FACTOR" value="FALSE" />
<define name="CALC_AMSL_BARO" value="TRUE" />
</section>
<!-- local magnetic field -->
<!-- http://wiki.paparazziuav.org/wiki/Subsystem/ahrs#Local_Magnetic_Field -->
<section name="AHRS" prefix="AHRS_">
<!-- values used if no GPS fix, on 3D fix is update by geo_mag module -->
<!-- Toulouse -->
<!--define name="H_X" value="0.513081"/>
<define name="H_Y" value="-0.00242783"/>
<define name="H_Z" value="0.858336"/-->
<!-- Delft -->
<define name="H_X" value="0.3892503" />
<define name="H_Y" value="0.0017972" />
<define name="H_Z" value="0.9211303" />
</section>
<section name="INS" prefix="INS_">
<define name="SONAR_MAX_RANGE" value="2.2" />
<define name="SONAR_UPDATE_ON_AGL" value="TRUE" />
</section>
<section name="RC_SETPOINT" prefix="STABILIZATION_ATTITUDE_">
<!-- setpoint limits for attitude stabilization rc flight -->
<define name="SP_MAX_PHI" value="45" unit="deg" />
<define name="SP_MAX_THETA" value="45" unit="deg" />
<define name="SP_MAX_R" value="300" unit="deg/s" />
<define name="DEADBAND_A" value="0" />
<define name="DEADBAND_E" value="0" />
<define name="DEADBAND_R" value="50" />
</section>
<section name="ATTITUDE_REFERENCE" prefix="STABILIZATION_ATTITUDE_">
<!-- attitude reference generation model -->
<define name="REF_OMEGA_P" value="450" unit="deg/s" />
<define name="REF_ZETA_P" value="0.9" />
<define name="REF_MAX_P" value="600." unit="deg/s" />
<define name="REF_MAX_PDOT" value="RadOfDeg(8000.)" />
<define name="REF_OMEGA_Q" value="450" unit="deg/s" />
<define name="REF_ZETA_Q" value="0.9" />
<define name="REF_MAX_Q" value="600." unit="deg/s" />
<define name="REF_MAX_QDOT" value="RadOfDeg(8000.)" />
<define name="REF_OMEGA_R" value="450" unit="deg/s" />
<define name="REF_ZETA_R" value="0.9" />
<define name="REF_MAX_R" value="600." unit="deg/s" />
<define name="REF_MAX_RDOT" value="RadOfDeg(8000.)" />
</section>
<section name="STABILIZATION_ATTITUDE_INDI" prefix="STABILIZATION_INDI_">
<!-- control effectiveness -->
<define name="G1_P" value="0.017" />
<define name="G1_Q" value="0.019" />
<define name="G1_R" value="0.0011" />
<define name="G2_R" value="0.089" />
<!-- For the bebop2 we need to filter the roll rate due to the dampers -->
<define name="FILTER_ROLL_RATE" value="FALSE" />
<define name="FILTER_PITCH_RATE" value="FALSE" />
<define name="FILTER_YAW_RATE" value="FALSE" />
<!-- reference acceleration for attitude control -->
<define name="REF_ERR_P" value="100.0" />
<define name="REF_ERR_Q" value="100.0" />
<define name="REF_ERR_R" value="100.0" />
<define name="REF_RATE_P" value="14.0" />
<define name="REF_RATE_Q" value="14.0" />
<define name="REF_RATE_R" value="14.0" />
<!-- second order filter parameters -->
<define name="FILT_OMEGA" value="20.0" />
<define name="FILT_ZETA" value="0.55" />
<define name="FILT_OMEGA_R" value="20.0" />
<define name="FILT_ZETA_R" value="0.55" />
<!-- first order actuator dynamics -->
<define name="ACT_DYN_P" value="0.04" />
<define name="ACT_DYN_Q" value="0.04" />
<define name="ACT_DYN_R" value="0.04" />
<!-- Adaptive Learning Rate -->
<define name="USE_ADAPTIVE" value="FALSE" />
<define name="ADAPTIVE_MU" value="0.0001" />
</section>
<section name="GUIDANCE_V" prefix="GUIDANCE_V_">
<define name="HOVER_KP" value="350" />
<define name="HOVER_KD" value="85" />
<define name="HOVER_KI" value="20" />
<define name="NOMINAL_HOVER_THROTTLE" value="0.4" />
<define name="ADAPT_THROTTLE_ENABLED" value="FALSE" />
</section>
<section name="GUIDANCE_H" prefix="GUIDANCE_H_">
<!-- Good weather -->
<define name="MAX_BANK" value="20" unit="deg" />
<define name="REF_MAX_SPEED" value="2" unit="m/s" />
<!-- Bad weather -->
<!-- define name="MAX_BANK" value="32" unit="deg"/ -->
<define name="PGAIN" value="120" />
<define name="DGAIN" value="100" />
<define name="IGAIN" value="30" />
</section>
<section name="NAVIGATION" prefix="NAV_">
<define name="CLIMB_VSPEED" value="4.5" />
<define name="DESCEND_VSPEED" value="-1.0" />
</section>
<section name="SIMULATOR" prefix="NPS_">
<define name="ACTUATOR_NAMES" value="nw_motor, ne_motor, se_motor, sw_motor" type="string[]" />
<define name="JSBSIM_MODEL" value="simple_x_quad_ccw" type="string" />
<define name="SENSORS_PARAMS" value="nps_sensors_params_default.h" type="string" />
</section>
<section name="AUTOPILOT">
<define name="MODE_STARTUP" value="AP_MODE_RC_DIRECT" />
<define name="MODE_MANUAL" value="AP_MODE_RC_DIRECT" /> <!-- changing this mode may not work, since fbw will be in mode manual directly from rc!-->
<define name="MODE_AUTO1" value="AP_MODE_ATTITUDE_DIRECT" />
<define name="MODE_AUTO2" value="AP_MODE_ATTITUDE_DIRECT" />
<define name="NO_RC_THRUST_LIMIT" value="TRUE" />
</section>
<section name="BAT">
<define name="MILLIAMP_AT_FULL_THROTTLE" value="8700" />
<define name="CATASTROPHIC_BAT_LEVEL" value="9.9" unit="V" />
<define name="CRITIC_BAT_LEVEL" value="10.8" unit="V" />
<define name="LOW_BAT_LEVEL" value="11.1" unit="V" />
<define name="MAX_BAT_LEVEL" value="12.4" unit="V" />
</section>
</airframe>
+230
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@@ -0,0 +1,230 @@
<!DOCTYPE airframe SYSTEM "../airframe.dtd">
<?xml version="1.0" encoding="UTF-8"?>
<!-- this is a quadrotor frame equiped with
* Autopilot: 3dr Pixhawk 2.4
* IMU: MPU6000
* Actuators: PWM motor controllers
* GPS: Ublox http://wiki.paparazziuav.org/wiki/Subsystem/gps
* RC: PPM
-->
<airframe name="iris_pid">
<firmware name="rotorcraft">
<target name="ap" board="px4fmu_2.4" />
<define name="BAT_CHECKER_DELAY" value="80" />
<!-- amount of time it take for the bat to check -->
<!-- to avoid bat low spike detection when strong pullup withch draws short sudden power-->
<define name="CATASTROPHIC_BATTERY_KILL_DELAY" value="80" />
<!-- in seconds-->
<target name="nps" board="pc">
<subsystem name="fdm" type="jsbsim" />
<subsystem name="udp" />
</target>
<subsystem name="telemetry" type="transparent" />
<subsystem name="imu" type="mpu6000">
<!-- <subsystem name="imu" type="L3GD20">-->
<configure name="IMU_MPU_SPI_DEV" value="spi1" />
<configure name="IMU_MPU_SPI_SLAVE_IDX" value="SPI_SLAVE2" />
</subsystem>
<subsystem name="gps" type="ublox" />
<subsystem name="stabilization" type="int_quat" />
<subsystem name="ahrs" type="int_cmpl_quat" />
<subsystem name="ins" type="extended" />
<subsystem name="current_sensor">
<configure name="ADC_CURRENT_SENSOR" value="ADC_3" />
</subsystem>
<subsystem name="intermcu" type="uart">
<configure name="INTERMCU_PORT" value="UART6" />
<configure name="INTERMCU_BAUD" value="B1500000" />
</subsystem>
</firmware>
<firmware name="rotorcraft">
<target name="fbw" board="px4io_2.4" />
<subsystem name="motor_mixing" />
<subsystem name="radio_control" type="ppm">
<define name="USE_KILL_SWITCH_FOR_MOTOR_ARMING" value="1" />
<define name="RADIO_KILL_SWITCH" value="RADIO_KILL" />
</subsystem>
<!-- <subsystem name="radio_control" type="spektrum">-->
<!-- <define name="RADIO_CONTROL_SPEKTRUM_NO_SIGN" value="1"/>-->
<!-- <define name="USE_KILL_SWITCH_FOR_MOTOR_ARMING" value="1"/>-->
<!-- <define name="RADIO_FBW_MODE" value="RADIO_AUX2"/>-->
<!-- <define name="RADIO_MODE" value="RADIO_GEAR"/>-->
<!-- <define name="SPEKTRUM_HAS_SOFT_BIND_PIN" value="1"/>-->
<!-- </subsystem>-->
<subsystem name="actuators" type="pwm">
<define name="SERVO_HZ" value="400" />
</subsystem>
<define name="RC_LOST_FBW_MODE" value="FBW_MODE_FAILSAFE" />
<!-- Switch to Failsafe or to Autopilot on RC loss? -->
<define name="RC_LOST_IN_AUTO_FBW_MODE" value="FBW_MODE_AUTO" />
<define name="AP_LOST_FBW_MODE" value="FBW_MODE_MANUAL" />
<!-- Switch to Failsafe or to Manual on AP loss? -->
<define name="INTERMCU_LOST_CNT" value="100" />
<subsystem name="intermcu" type="uart">
<configure name="INTERMCU_PORT" value="UART2" />
<configure name="INTERMCU_BAUD" value="B1500000" />
</subsystem>
</firmware>
<firmware name="test_progs">
<target name="test_telemetry" board="px4fmu_2.4" />
</firmware>
<firmware name="test_progs">
<target name="test_baro_board" board="px4fmu_2.4" />
</firmware>
<firmware name="test_progs">
<target name="test_datalink" board="px4fmu_2.4" />
</firmware>
<modules main_freq="512">
<load name="px4io_flash.xml" />
<load name="geo_mag.xml" />
<load name="air_data.xml" />
<load name="send_imu_mag_current.xml" />
<load name="gps_ubx_ucenter.xml" />
<!-- <load name="spektrum_soft_bind.xml"/>-->
</modules>
<section name="MISC">
<define name="MilliAmpereOfAdc(adc)" value="((float)adc) * (3.3f / 4096.0f) * (90.0f / 5.0f)" />
<!-- 100Amp = 2Volt -> 2482,42 tick/100Amp"(0.0402832*adc)" -->
</section>
<section name="IMU" prefix="IMU_">
<!-- replace this with your own calibration -->
<define name="MAG_X_NEUTRAL" value="14" />
<define name="MAG_Y_NEUTRAL" value="116" />
<define name="MAG_Z_NEUTRAL" value="119" />
<define name="MAG_X_SENS" value="5.09245681612" integer="16" />
<define name="MAG_Y_SENS" value="5.29702744632" integer="16" />
<define name="MAG_Z_SENS" value="5.65287938992" integer="16" />
<define name="BODY_TO_IMU_PHI" value="180." unit="deg" />
<define name="BODY_TO_IMU_THETA" value="180." unit="deg" />
<define name="BODY_TO_IMU_PSI" value="90." unit="deg" />
</section>
<commands>
<axis name="PITCH" failsafe_value="0" />
<axis name="ROLL" failsafe_value="0" />
<axis name="YAW" failsafe_value="0" />
<axis name="THRUST" failsafe_value="0" />
</commands>
<rc_commands>
<set command="THRUST" value="@THROTTLE" />
<set command="ROLL" value="@ROLL" />
<set command="PITCH" value="@PITCH" />
<set command="YAW" value="@YAW" />
</rc_commands>
<servos driver="Default">
<servo name="TOP_LEFT" no="2" min="1140" neutral="1280" max="1850" />
<servo name="TOP_RIGHT" no="0" min="1140" neutral="1280" max="1850" />
<servo name="BOTTOM_RIGHT" no="3" min="1140" neutral="1280" max="1850" />
<servo name="BOTTOM_LEFT" no="1" min="1140" neutral="1280" max="1850" />
</servos>
<section name="MIXING" prefix="MOTOR_MIXING_">
<define name="TRIM_ROLL" value="0" />
<define name="TRIM_PITCH" value="0" />
<define name="TRIM_YAW" value="0" />
<define name="REVERSE" value="FALSE" />
<define name="TYPE" value="QUAD_X" />
</section>
<command_laws>
<call fun="motor_mixing_run(autopilot_motors_on,FALSE,values)" />
<set servo="TOP_LEFT" value="motor_mixing.commands[MOTOR_FRONT_LEFT]" />
<set servo="TOP_RIGHT" value="motor_mixing.commands[MOTOR_FRONT_RIGHT]" />
<set servo="BOTTOM_RIGHT" value="motor_mixing.commands[MOTOR_BACK_RIGHT]" />
<set servo="BOTTOM_LEFT" value="motor_mixing.commands[MOTOR_BACK_LEFT]" />
</command_laws>
<section name="AIR_DATA" prefix="AIR_DATA_">
<define name="CALC_AIRSPEED" value="FALSE" />
<define name="CALC_TAS_FACTOR" value="FALSE" />
<define name="CALC_AMSL_BARO" value="TRUE" />
</section>
<!-- local magnetic field -->
<!-- http://wiki.paparazziuav.org/wiki/Subsystem/ahrs#Local_Magnetic_Field -->
<section name="AHRS" prefix="AHRS_">
<!-- values used if no GPS fix, on 3D fix is update by geo_mag module -->
<!-- Toulouse -->
<!--define name="H_X" value="0.513081"/>
<define name="H_Y" value="-0.00242783"/>
<define name="H_Z" value="0.858336"/-->
<!-- Delft -->
<define name="H_X" value="0.3892503" />
<define name="H_Y" value="0.0017972" />
<define name="H_Z" value="0.9211303" />
</section>
<section name="INS" prefix="INS_">
<define name="SONAR_MAX_RANGE" value="2.2" />
<define name="SONAR_UPDATE_ON_AGL" value="TRUE" />
</section>
<section name="STABILIZATION_ATTITUDE" prefix="STABILIZATION_ATTITUDE_">
<!-- setpoints -->
<define name="SP_MAX_PHI" value="45." unit="deg" />
<define name="SP_MAX_THETA" value="45." unit="deg" />
<define name="SP_MAX_R" value="90." unit="deg/s" />
<define name="DEADBAND_R" value="250" />
<!-- reference -->
<define name="REF_OMEGA_P" value="800" unit="deg/s" />
<define name="REF_ZETA_P" value="0.85" />
<define name="REF_MAX_P" value="300." unit="deg/s" />
<define name="REF_MAX_PDOT" value="RadOfDeg(7000.)" />
<define name="REF_OMEGA_Q" value="800" unit="deg/s" />
<define name="REF_ZETA_Q" value="0.85" />
<define name="REF_MAX_Q" value="300." unit="deg/s" />
<define name="REF_MAX_QDOT" value="RadOfDeg(7000.)" />
<define name="REF_OMEGA_R" value="500" unit="deg/s" />
<define name="REF_ZETA_R" value="0.85" />
<define name="REF_MAX_R" value="180." unit="deg/s" />
<define name="REF_MAX_RDOT" value="RadOfDeg(1800.)" />
<!-- feedback -->
<define name="PHI_PGAIN" value="900" />
<define name="PHI_DGAIN" value="200" />
<define name="PHI_IGAIN" value="200" />
<define name="THETA_PGAIN" value="900" />
<define name="THETA_DGAIN" value="200" />
<define name="THETA_IGAIN" value="200" />
<define name="PSI_PGAIN" value="900" />
<define name="PSI_DGAIN" value="200" />
<define name="PSI_IGAIN" value="10" />
<!-- feedforward -->
<define name="PHI_DDGAIN" value="75" />
<define name="THETA_DDGAIN" value="75" />
<define name="PSI_DDGAIN" value="75" />
</section>
<section name="GUIDANCE_V" prefix="GUIDANCE_V_">
<define name="HOVER_KP" value="350" />
<define name="HOVER_KD" value="85" />
<define name="HOVER_KI" value="20" />
<define name="NOMINAL_HOVER_THROTTLE" value="0.4" />
<define name="ADAPT_THROTTLE_ENABLED" value="FALSE" />
</section>
<section name="GUIDANCE_H" prefix="GUIDANCE_H_">
<!-- Good weather -->
<define name="MAX_BANK" value="20" unit="deg" />
<define name="REF_MAX_SPEED" value="2" unit="m/s" />
<!-- Bad weather -->
<!-- define name="MAX_BANK" value="32" unit="deg"/ -->
<define name="PGAIN" value="120" />
<define name="DGAIN" value="100" />
<define name="IGAIN" value="30" />
</section>
<section name="NAVIGATION" prefix="NAV_">
<define name="CLIMB_VSPEED" value="4.5" />
<define name="DESCEND_VSPEED" value="-1.0" />
</section>
<section name="SIMULATOR" prefix="NPS_">
<define name="ACTUATOR_NAMES" value="nw_motor, ne_motor, se_motor, sw_motor" type="string[]" />
<define name="JSBSIM_MODEL" value="simple_x_quad_ccw" type="string" />
<define name="SENSORS_PARAMS" value="nps_sensors_params_default.h" type="string" />
</section>
<section name="AUTOPILOT">
<define name="MODE_STARTUP" value="AP_MODE_RC_DIRECT" />
<define name="MODE_MANUAL" value="AP_MODE_RC_DIRECT" />
<define name="MODE_AUTO1" value="AP_MODE_ATTITUDE_DIRECT" />
<define name="MODE_AUTO2" value="AP_MODE_ATTITUDE_DIRECT" />
<define name="NO_RC_THRUST_LIMIT" value="TRUE" />
</section>
<section name="BAT">
<define name="MILLIAMP_AT_FULL_THROTTLE" value="8700" />
<define name="CATASTROPHIC_BAT_LEVEL" value="9.9" unit="V" />
<define name="CRITIC_BAT_LEVEL" value="10.8" unit="V" />
<define name="LOW_BAT_LEVEL" value="11.1" unit="V" />
<define name="MAX_BAT_LEVEL" value="12.4" unit="V" />
</section>
</airframe>
+60
View File
@@ -0,0 +1,60 @@
<?xml version="1.0"?>
<!-- $Id$
--
-- (c) 2006 Pascal Brisset, Antoine Drouin
--
-- This file is part of paparazzi.
--
-- paparazzi is free software; you can redistribute it and/or modify
-- it under the terms of the GNU General Public License as published by
-- the Free Software Foundation; either version 2, or (at your option)
-- any later version.
--
-- paparazzi is distributed in the hope that it will be useful,
-- but WITHOUT ANY WARRANTY; without even the implied warranty of
-- MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
-- GNU General Public License for more details.
--
-- You should have received a copy of the GNU General Public License
-- along with paparazzi; see the file COPYING. If not, write to
-- the Free Software Foundation, 59 Temple Place - Suite 330,
-- Boston, MA 02111-1307, USA.
-->
<!--
-- Attributes of root (Radio) tag :
-- name: name of RC
-- data_min: min width of a pulse to be considered as a data pulse
-- data_max: max width of a pulse to be considered as a data pulse
-- sync_min: min width of a pulse to be considered as a synchro pulse
-- sync_max: max width of a pulse to be considered as a synchro pulse
-- pulse_type: POSITIVE ( Futaba and others) | NEGATIVE (JR)
-- min, max and sync are expressed in micro-seconds
-->
<!--
-- Attributes of channel tag :
-- ctl: name of the command on the transmitter - only for displaying
-- function: logical command
-- average: (boolean) channel filtered through several frames (for discrete commands)
-- min: minimum pulse length (micro-seconds)
-- max: maximum pulse length (micro-seconds)
-- neutral: neutral pulse length (micro-seconds)
-- Note: a command may be reversed by exchanging min and max values
-->
<!DOCTYPE radio SYSTEM "radio.dtd">
<!-- Values set by experiment using X8R receiver SBus connection -->
<radio name="FrSky X9D + X8R receiver SBus connection" data_min="350" data_max="2500" sync_min ="8000" sync_max ="19000" pulse_type="POSITIVE">
<channel ctl="D" function="ROLL" min="990" neutral="1490" max="2015" average="0"/>
<channel ctl="C" function="PITCH" min="990" neutral="1490" max="2015" average="0"/>
<channel ctl="A" function="THROTTLE" min="990" neutral="990" max="2015" average="0"/>
<channel ctl="B" function="YAW" min="990" neutral="1490" max="2015" average="0"/>
<channel ctl="RSwtiches_Mix" function="MODE" min="1145" neutral="1500" max="1862" average="1"/>
<channel ctl="TILT" function="AUX2" min="990" neutral="990" max="2015" average="0"/>
<channel ctl="CH7" function="KILL" min="990" neutral="1490" max="2015" average="1"/>
<channel ctl="E" function="UNUSED2" min="990" neutral="1900" max="2015" average="1"/>
</radio>
@@ -20,6 +20,9 @@ SUBSYSTEM=="tty", ATTRS{product}=="FT232R USB UART", SYMLINK+="ftdi-serial", GRO
# Paparazzi STM32 Autopilot board USB CDC serial device
SUBSYSTEM=="tty", ATTRS{manufacturer}=="Paparazzi UAV", ATTRS{product}=="CDC Serial STM32", SYMLINK+="paparazzi/stm32-usb-serial"
# Paparazzi 3dr radio
SUBSYSTEM=="tty", ATTRS{idVendor}=="0403", ATTRS{idProduct}=="6015", SYMLINK+="paparazzi/link", GROUP="plugdev"
# MaxStream xbee pro box
SUBSYSTEM=="tty", ATTRS{product}=="MaxStream PKG-U", SYMLINK+="paparazzi/xbee", GROUP="plugdev"
+1 -1
View File
@@ -1,5 +1,5 @@
<?xml version="1.0"?>
<!DOCTYPE telemetry SYSTEM "telemetry.dtd">
<!DOCTYPE telemetry SYSTEM "../telemetry.dtd">
<telemetry>
<process name="Ap">
<mode name="default">