pni micromag for fixed wing

This commit is contained in:
Martin Mueller
2010-10-21 19:14:39 +00:00
parent 38120e1b4e
commit 89c8fd5c73
11 changed files with 765 additions and 176 deletions
+50 -20
View File
@@ -5,11 +5,11 @@
PerkinElmer TPS334 IR Sensors
Tilted infrared sensor (http://paparazzi.enac.fr/wiki/index.php/Image:Tiny_v2_1_Funjet.jpg)
XBee modem
Payload: Sensirion humidity/temp, VTI pressure/temp
K66, LEA 4P
Payload: Sensirion humidity/temp, VTI pressure/temp, ETS airspeed
LEA 4P
-->
<airframe name="Funjet FMI 1 K66">
<airframe name="Funjet FMI 1">
<!-- commands section -->
<servos>
@@ -37,7 +37,7 @@
<command_laws>
<let var="aileron" value="@ROLL * AILEVON_AILERON_RATE"/>
<let var="elevator" value="@PITCH * AILEVON_ELEVATOR_RATE"/>
<let var="elevator" value="@PITCH * AILEVON_ELEVATOR_RATE"/>
<set servo="MOTOR" value="@THROTTLE"/>
<set servo="AILEVON_LEFT" value="$elevator + $aileron"/>
<set servo="AILEVON_RIGHT" value="$elevator - $aileron"/>
@@ -83,9 +83,9 @@
<define name="CATASTROPHIC_BAT_LEVEL" value="9.3" unit="V"/>
<!-- 0.0247311828 -->
<!-- 0.02432905 -->
<define name="VoltageOfAdc(adc)" value="(0.02454*adc)"/>
<define name="VoltageOfAdc(adc)" value="(0.02454*adc)"/>
</section>
<section name="MISC">
<define name="NOMINAL_AIRSPEED" value="15." unit="m/s"/>
<define name="CARROT" value="5." unit="s"/>
@@ -97,8 +97,9 @@
<define name="TRIGGER_DELAY" value="1."/>
<define name="DEFAULT_CIRCLE_RADIUS" value="120."/>
<define name="MIN_CIRCLE_RADIUS" value="50."/>
</section>
<section name="VERTICAL CONTROL" prefix="V_CTL_">
<define name="POWER_CTL_BAT_NOMINAL" value="11.1" unit="volt"/>
@@ -164,9 +165,9 @@
<section name="FAILSAFE" prefix="FAILSAFE_">
<define name="DELAY_WITHOUT_GPS" value="2" unit="s"/>
<define name="DEFAULT_THROTTLE" value="0.3" unit="%"/>
<define name="DEFAULT_ROLL" value="0.3" unit="rad"/>
<define name="DEFAULT_PITCH" value="0.5" unit="rad"/>
<define name="DEFAULT_THROTTLE" value="0.3" unit="%"/>
<define name="DEFAULT_ROLL" value="0.3" unit="rad"/>
<define name="DEFAULT_PITCH" value="0.5" unit="rad"/>
<define name="HOME_RADIUS" value="100" unit="m"/>
</section>
@@ -174,11 +175,31 @@
<define name="DEVICE_TYPE" value="XBEE"/>
<define name="DEVICE_ADDRESS" value="...."/>
</section>
<section name="SIMU">
<define name="YAW_RESPONSE_FACTOR" value="0.5"/>
</section>
<section name="MICROMAG">
<define name="MM_SS_PIN" value="20"/>
<define name="MM_SS_IODIR" value="IO0DIR"/>
<define name="MM_SS_IOSET" value="IO0SET"/>
<define name="MM_SS_IOCLR" value="IO0CLR"/>
<define name="MM_RESET_PIN" value="29"/>
<define name="MM_RESET_IODIR" value="IO0DIR"/>
<define name="MM_RESET_IOSET" value="IO0SET"/>
<define name="MM_RESET_IOCLR" value="IO0CLR"/>
<define name="MM_DRDY_PINSEL" value="PINSEL1"/>
<define name="MM_DRDY_PINSEL_BIT" value="0"/>
<define name="MM_DRDY_PINSEL_VAL" value="1"/>
<define name="MM_DRDY_EINT" value="0"/>
<define name="MM_DRDY_VIC_IT" value="VIC_EINT0"/>
</section>
<makefile>
CONFIG = \"tiny_2_1.h\"
@@ -195,7 +216,7 @@ ap.CFLAGS += -DACTUATORS=\"servos_4017_hw.h\" -DSERVOS_4017
ap.srcs += $(SRC_ARCH)/servos_4017_hw.c actuators.c
ap.CFLAGS += -DRADIO_CONTROL
ap.srcs += radio_control.c $(SRC_ARCH)/ppm_hw.c
ap.srcs += radio_control.c $(SRC_ARCH)/ppm_hw.c
ap.CFLAGS += -DDOWNLINK -DUSE_UART1 -DDOWNLINK_TRANSPORT=XBeeTransport -DXBEE_UART=Uart1 -DDATALINK=XBEE -DUART1_BAUD=B57600
ap.srcs += downlink.c $(SRC_ARCH)/uart_hw.c datalink.c xbee.c
@@ -206,7 +227,7 @@ ap.srcs += downlink.c $(SRC_ARCH)/uart_hw.c datalink.c xbee.c
ap.CFLAGS += -DINTER_MCU
ap.srcs += inter_mcu.c
ap.srcs += inter_mcu.c
ap.CFLAGS += -DADC -DUSE_ADC_0 -DUSE_ADC_1 -DUSE_ADC_2
ap.srcs += $(SRC_ARCH)/adc_hw.c
@@ -225,22 +246,31 @@ ap.srcs += nav_line.c
ap.srcs += nav_survey_rectangle.c
ap.srcs += humid_sht.c
ap.CFLAGS += -DUSE_HUMID_SHT -DDAT_PIN=3 -DSCK_PIN=2
ap.CFLAGS += -DUSE_HUMID_SHT -DDAT_PIN=30 -DSCK_PIN=4
ap.CFLAGS += -DUSE_I2C0
ap.srcs += i2c.c $(SRC_ARCH)/i2c_hw.c
ap.CFLAGS += -DUSE_AIRSPEED_ETS
ap.srcs += airspeed_ets_o.c
ap.CFLAGS += -DUSE_IR_MLX
ap.srcs += ir_mlx.c
ap.srcs += baro_scp.c
ap.CFLAGS += -DUSE_BARO_SCP
ap.srcs += baro_scp_i2c.c
ap.srcs += joystick.c
ap.CFLAGS += -DUSE_JOYSTICK
#ap.CFLAGS += -DUSE_MAG_HMC
#ap.srcs += mag_hmc5843.c
ap.CFLAGS += -DMICROMAG_DRDY_VIC_SLOT=12 -DSSP_VIC_SLOT=11 -DUSE_MICROMAG_FW
ap.srcs += micromag_fw.c $(SRC_ARCH)/micromag_fw_hw.c
# Config for SITL simulation
include $(PAPARAZZI_SRC)/conf/autopilot/sitl.makefile
sim.CFLAGS += -DBOARD_CONFIG=\"tiny.h\" -DAGR_CLIMB -DLOITER_TRIM -DALT_KALMAN
sim.srcs += nav_line.c nav_survey_rectangle.c
sim.srcs += joystick.c
sim.CFLAGS += -DUSE_JOYSTICK
</makefile>
</airframe>
+272
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@@ -0,0 +1,272 @@
<!DOCTYPE airframe SYSTEM "airframe.dtd">
<!-- Funjet Multiplex (http://www.multiplex-rc.de/), Jeti ECO 25
Tiny 2.11 board (http://paparazzi.enac.fr/wiki/index.php/Tiny_v2)
Tilted infrared sensor (http://paparazzi.enac.fr/wiki/index.php/Image:Tiny_v2_1_Funjet.jpg)
XBee modem
Payload: Sensirion humidity/temp, VTI pressure/temp, ETS airspeed
LEA 5H
-->
<airframe name="Funjet FMI 2">
<!-- commands section -->
<servos>
<servo name="MOTOR" no="0" min="1000" neutral="1000" max="2000"/>
<servo name="AILEVON_LEFT" no="2" min="1900" neutral="1500" max="1100"/>
<servo name="AILEVON_RIGHT" no="6" min="1100" neutral="1500" max="1900"/>
</servos>
<commands>
<axis name="THROTTLE" failsafe_value="0"/>
<axis name="ROLL" failsafe_value="0"/>
<axis name="PITCH" failsafe_value="0"/>
</commands>
<rc_commands>
<set command="THROTTLE" value="@THROTTLE"/>
<set command="ROLL" value="@ROLL"/>
<set command="PITCH" value="@PITCH"/>
</rc_commands>
<section name="MIXER">
<define name="AILEVON_AILERON_RATE" value="0.45"/>
<define name="AILEVON_ELEVATOR_RATE" value="0.8"/>
</section>
<command_laws>
<let var="aileron" value="@ROLL * AILEVON_AILERON_RATE"/>
<let var="elevator" value="@PITCH * AILEVON_ELEVATOR_RATE"/>
<set servo="MOTOR" value="@THROTTLE"/>
<set servo="AILEVON_LEFT" value="$elevator + $aileron"/>
<set servo="AILEVON_RIGHT" value="$elevator - $aileron"/>
</command_laws>
<section name="AUTO1" prefix="AUTO1_">
<define name="MAX_ROLL" value="0.85"/>
<define name="MAX_PITCH" value="0.6"/>
</section>
<section name="adc" prefix="ADC_CHANNEL_">
<define name="IR1" value="ADC_1"/>
<define name="IR2" value="ADC_2"/>
<define name="IR_TOP" value="ADC_0"/>
<define name="IR_NB_SAMPLES" value="16"/>
</section>
<section name="INFRARED" prefix="IR_">
<define name="ADC_IR1_NEUTRAL" value="512"/>
<define name="ADC_IR2_NEUTRAL" value="512"/>
<define name="ADC_TOP_NEUTRAL" value="512"/>
<define name="CORRECTION_UP" value="1."/>
<define name="CORRECTION_DOWN" value="1."/>
<define name="CORRECTION_LEFT" value="1."/>
<define name="CORRECTION_RIGHT" value="1."/>
<define name="LATERAL_CORRECTION" value="1"/>
<define name="LONGITUDINAL_CORRECTION" value="1"/>
<define name="VERTICAL_CORRECTION" value="1.5"/>
<define name="HORIZ_SENSOR_TILTED" value="1"/>
<define name="IR1_SIGN" value="-1"/>
<define name="IR2_SIGN" value="-1"/>
<define name="TOP_SIGN" value="1"/>
<define name="ROLL_NEUTRAL_DEFAULT" value="0" unit="deg"/>
<define name="PITCH_NEUTRAL_DEFAULT" value="0" unit="deg"/>
</section>
<section name="BAT">
<define name="MILLIAMP_AT_FULL_THROTTLE" value="10000."/>
<define name="CATASTROPHIC_BAT_LEVEL" value="9.3" unit="V"/>
<!-- 0.0247311828 -->
<!-- 0.02432905 -->
<define name="VoltageOfAdc(adc)" value="(0.02454*adc)"/>
</section>
<section name="MISC">
<define name="NOMINAL_AIRSPEED" value="15." unit="m/s"/>
<define name="CARROT" value="5." unit="s"/>
<define name="KILL_MODE_DISTANCE" value="(1.5*MAX_DIST_FROM_HOME)"/>
<define name="CONTROL_RATE" value="60" unit="Hz"/>
<!-- <define name="XBEE_INIT" value="\"ATPL2\rATRN1\rATTT80\r\""/> -->
<!-- <define name="NO_XBEE_API_INIT" value="TRUE"/> -->
<define name="ALT_KALMAN_ENABLED" value="FALSE"/>
<define name="TRIGGER_DELAY" value="1."/>
<define name="DEFAULT_CIRCLE_RADIUS" value="120."/>
<define name="MIN_CIRCLE_RADIUS" value="50."/>
</section>
<section name="VERTICAL CONTROL" prefix="V_CTL_">
<define name="POWER_CTL_BAT_NOMINAL" value="11.1" unit="volt"/>
<!-- outer loop proportional gain -->
<define name="ALTITUDE_PGAIN" value="-0.06"/> <!-- -0.024 -->
<!-- outer loop saturation -->
<define name="ALTITUDE_MAX_CLIMB" value="2."/>
<!-- auto throttle inner loop -->
<define name="AUTO_THROTTLE_NOMINAL_CRUISE_THROTTLE" value="0.45"/>
<define name="AUTO_THROTTLE_MIN_CRUISE_THROTTLE" value="0.35"/>
<define name="AUTO_THROTTLE_MAX_CRUISE_THROTTLE" value="0.85"/>
<define name="AUTO_THROTTLE_LOITER_TRIM" value="1000"/>
<define name="AUTO_THROTTLE_DASH_TRIM" value="-1200"/>
<define name="AUTO_THROTTLE_CLIMB_THROTTLE_INCREMENT" value="0.2" unit="%/(m/s)"/>
<define name="AUTO_THROTTLE_PGAIN" value="-0.023"/> <!-- -0.012 -->
<define name="AUTO_THROTTLE_IGAIN" value="0.01"/>
<define name="AUTO_THROTTLE_PITCH_OF_VZ_PGAIN" value="0.05"/>
<!-- auto pitch inner loop -->
<define name="AUTO_PITCH_PGAIN" value="-0.06"/> <!-- -0.03 -->
<define name="AUTO_PITCH_IGAIN" value="0.0"/>
<define name="AUTO_PITCH_MAX_PITCH" value="0.35"/>
<define name="AUTO_PITCH_MIN_PITCH" value="-0.35"/>
<define name="THROTTLE_SLEW" value="0.1"/>
</section>
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN" value="-0.9"/>
<define name="ROLL_MAX_SETPOINT" value="0.70" unit="radians"/> <!-- 0.5 -->
<define name="PITCH_MAX_SETPOINT" value="0.5" unit="radians"/>
<define name="PITCH_MIN_SETPOINT" value="-0.5" unit="radians"/>
<define name="ROLL_PGAIN" value="6600."/>
<define name="AILERON_OF_THROTTLE" value="0.0"/>
<define name="PITCH_PGAIN" value="-5500."/>
<define name="PITCH_DGAIN" value="0.4"/>
<define name="ELEVATOR_OF_ROLL" value="2400"/>
<!--define name="ROLL_ATTITUDE_GAIN" value="-7500"/>
<define name="ROLL_RATE_GAIN" value="-1500"/-->
</section>
<section name="NAV">
<define name="NAV_PITCH" value="0."/>
<define name="NAV_GLIDE_PITCH_TRIM" value="0"/>
</section>
<section name="AGGRESSIVE" prefix="AGR_">
<define name="BLEND_START" value="50"/><!-- Altitude Error to Initiate Aggressive Climb CANNOT BE ZERO!!-->
<define name="BLEND_END" value="15"/><!-- Altitude Error to Blend Aggressive to Regular Climb Modes CANNOT BE ZERO!!-->
<define name="CLIMB_THROTTLE" value="0.9"/><!-- Gaz for Aggressive Climb -->
<define name="CLIMB_PITCH" value="0.35"/><!-- Pitch for Aggressive Climb -->
<define name="DESCENT_THROTTLE" value="0.05"/><!-- Gaz for Aggressive Decent -->
<define name="DESCENT_PITCH" value="-0.35"/><!-- Pitch for Aggressive Decent -->
<define name="CLIMB_NAV_RATIO" value="0.8"/><!-- Percent Navigation for Altitude Error Equal to Start Altitude -->
<define name="DESCENT_NAV_RATIO" value="1.0"/>
</section>
<section name="FAILSAFE" prefix="FAILSAFE_">
<define name="DELAY_WITHOUT_GPS" value="2" unit="s"/>
<define name="DEFAULT_THROTTLE" value="0.3" unit="%"/>
<define name="DEFAULT_ROLL" value="0.3" unit="rad"/>
<define name="DEFAULT_PITCH" value="0.5" unit="rad"/>
<define name="HOME_RADIUS" value="100" unit="m"/>
</section>
<section name="DATALINK" prefix="DATALINK_">
<define name="DEVICE_TYPE" value="XBEE"/>
<define name="DEVICE_ADDRESS" value="...."/>
</section>
<section name="SIMU">
<define name="YAW_RESPONSE_FACTOR" value="0.5"/>
</section>
<section name="MICROMAG">
<define name="MM_SS_PIN" value="20"/>
<define name="MM_SS_IODIR" value="IO0DIR"/>
<define name="MM_SS_IOSET" value="IO0SET"/>
<define name="MM_SS_IOCLR" value="IO0CLR"/>
<define name="MM_RESET_PIN" value="29"/>
<define name="MM_RESET_IODIR" value="IO0DIR"/>
<define name="MM_RESET_IOSET" value="IO0SET"/>
<define name="MM_RESET_IOCLR" value="IO0CLR"/>
<define name="MM_DRDY_PINSEL" value="PINSEL1"/>
<define name="MM_DRDY_PINSEL_BIT" value="0"/>
<define name="MM_DRDY_PINSEL_VAL" value="1"/>
<define name="MM_DRDY_EINT" value="0"/>
<define name="MM_DRDY_VIC_IT" value="VIC_EINT0"/>
</section>
<makefile>
CONFIG = \"tiny_2_1.h\"
include $(PAPARAZZI_SRC)/conf/autopilot/tiny.makefile
FLASH_MODE=IAP
ap.CFLAGS += -DFBW -DAP -DBOARD_CONFIG=$(CONFIG) -DLED -DTIME_LED=1
ap.srcs = sys_time.c $(SRC_ARCH)/sys_time_hw.c $(SRC_ARCH)/armVIC.c main_fbw.c main_ap.c main.c
ap.srcs += commands.c
ap.CFLAGS += -DACTUATORS=\"servos_4017_hw.h\" -DSERVOS_4017
ap.srcs += $(SRC_ARCH)/servos_4017_hw.c actuators.c
ap.CFLAGS += -DRADIO_CONTROL
ap.srcs += radio_control.c $(SRC_ARCH)/ppm_hw.c
ap.CFLAGS += -DDOWNLINK -DUSE_UART1 -DDOWNLINK_TRANSPORT=XBeeTransport -DXBEE_UART=Uart1 -DDATALINK=XBEE -DUART1_BAUD=B57600
ap.srcs += downlink.c $(SRC_ARCH)/uart_hw.c datalink.c xbee.c
#TRANSPARENT
#ap.CFLAGS += -DDOWNLINK -DUSE_UART1 -DDOWNLINK_TRANSPORT=PprzTransport -DDOWNLINK_FBW_DEVICE=Uart1 -DDOWNLINK_AP_DEVICE=Uart1 -DPPRZ_UART=Uart1 -DDATALINK=PPRZ -DUART1_BAUD=B9600
#ap.srcs += downlink.c $(SRC_ARCH)/uart_hw.c datalink.c pprz_transport.c
ap.CFLAGS += -DINTER_MCU
ap.srcs += inter_mcu.c
ap.CFLAGS += -DADC -DUSE_ADC_0 -DUSE_ADC_1 -DUSE_ADC_2
ap.srcs += $(SRC_ARCH)/adc_hw.c
ap.CFLAGS += -DGPS -DUBX -DUSE_UART0 -DGPS_LINK=Uart0 -DUART0_BAUD=B38400 -DGPS_USE_LATLONG
# -DGPS_LED=2
ap.srcs += gps_ubx.c gps.c latlong.c
ap.CFLAGS += -DINFRARED -DALT_KALMAN -DWIND_INFO -DWIND_INFO_RET
ap.srcs += infrared.c estimator.c
ap.CFLAGS += -DNAV -DAGR_CLIMB -DLOITER_TRIM
ap.srcs += nav.c fw_h_ctl.c fw_v_ctl.c
ap.srcs += nav_line.c
ap.srcs += nav_survey_rectangle.c
ap.srcs += humid_sht.c
ap.CFLAGS += -DUSE_HUMID_SHT -DDAT_PIN=30 -DSCK_PIN=4
ap.CFLAGS += -DUSE_I2C0
ap.srcs += i2c.c $(SRC_ARCH)/i2c_hw.c
ap.CFLAGS += -DUSE_AIRSPEED_ETS
ap.srcs += airspeed_ets_o.c
ap.CFLAGS += -DUSE_IR_MLX
ap.srcs += ir_mlx.c
ap.CFLAGS += -DUSE_BARO_SCP
ap.srcs += baro_scp_i2c.c
ap.CFLAGS += -DMICROMAG_DRDY_VIC_SLOT=12 -DSSP_VIC_SLOT=11 -DUSE_MICROMAG_FW
ap.srcs += micromag_fw.c $(SRC_ARCH)/micromag_fw_hw.c
# Config for SITL simulation
include $(PAPARAZZI_SRC)/conf/autopilot/sitl.makefile
sim.CFLAGS += -DBOARD_CONFIG=\"tiny.h\" -DAGR_CLIMB -DLOITER_TRIM -DALT_KALMAN
sim.srcs += nav_line.c nav_survey_rectangle.c
</makefile>
</airframe>
+272
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@@ -0,0 +1,272 @@
<!DOCTYPE airframe SYSTEM "airframe.dtd">
<!-- Funjet Multiplex (http://www.multiplex-rc.de/), Jeti ECO 25
Tiny 2.11 board (http://paparazzi.enac.fr/wiki/index.php/Tiny_v2)
Tilted infrared sensor (http://paparazzi.enac.fr/wiki/index.php/Image:Tiny_v2_1_Funjet.jpg)
XBee modem
Payload: Sensirion humidity/temp, VTI pressure/temp, ETS airspeed
LEA 5H
-->
<airframe name="Funjet FMI 3">
<!-- commands section -->
<servos>
<servo name="MOTOR" no="0" min="1000" neutral="1000" max="2000"/>
<servo name="AILEVON_LEFT" no="2" min="1900" neutral="1515" max="1100"/>
<servo name="AILEVON_RIGHT" no="6" min="1100" neutral="1502" max="1900"/>
</servos>
<commands>
<axis name="THROTTLE" failsafe_value="0"/>
<axis name="ROLL" failsafe_value="0"/>
<axis name="PITCH" failsafe_value="0"/>
</commands>
<rc_commands>
<set command="THROTTLE" value="@THROTTLE"/>
<set command="ROLL" value="@ROLL"/>
<set command="PITCH" value="@PITCH"/>
</rc_commands>
<section name="MIXER">
<define name="AILEVON_AILERON_RATE" value="0.45"/>
<define name="AILEVON_ELEVATOR_RATE" value="0.8"/>
</section>
<command_laws>
<let var="aileron" value="@ROLL * AILEVON_AILERON_RATE"/>
<let var="elevator" value="@PITCH * AILEVON_ELEVATOR_RATE"/>
<set servo="MOTOR" value="@THROTTLE"/>
<set servo="AILEVON_LEFT" value="$elevator + $aileron"/>
<set servo="AILEVON_RIGHT" value="$elevator - $aileron"/>
</command_laws>
<section name="AUTO1" prefix="AUTO1_">
<define name="MAX_ROLL" value="0.85"/>
<define name="MAX_PITCH" value="0.6"/>
</section>
<section name="adc" prefix="ADC_CHANNEL_">
<define name="IR1" value="ADC_1"/>
<define name="IR2" value="ADC_2"/>
<define name="IR_TOP" value="ADC_0"/>
<define name="IR_NB_SAMPLES" value="16"/>
</section>
<section name="INFRARED" prefix="IR_">
<define name="ADC_IR1_NEUTRAL" value="512"/>
<define name="ADC_IR2_NEUTRAL" value="512"/>
<define name="ADC_TOP_NEUTRAL" value="512"/>
<define name="CORRECTION_UP" value="1."/>
<define name="CORRECTION_DOWN" value="1."/>
<define name="CORRECTION_LEFT" value="1."/>
<define name="CORRECTION_RIGHT" value="1."/>
<define name="LATERAL_CORRECTION" value="1"/>
<define name="LONGITUDINAL_CORRECTION" value="1"/>
<define name="VERTICAL_CORRECTION" value="1.5"/>
<define name="HORIZ_SENSOR_TILTED" value="1"/>
<define name="IR1_SIGN" value="-1"/>
<define name="IR2_SIGN" value="-1"/>
<define name="TOP_SIGN" value="1"/>
<define name="ROLL_NEUTRAL_DEFAULT" value="0" unit="deg"/>
<define name="PITCH_NEUTRAL_DEFAULT" value="0" unit="deg"/>
</section>
<section name="BAT">
<define name="MILLIAMP_AT_FULL_THROTTLE" value="10000."/>
<define name="CATASTROPHIC_BAT_LEVEL" value="9.3" unit="V"/>
<!-- 0.0247311828 -->
<!-- 0.02432905 -->
<define name="VoltageOfAdc(adc)" value="(0.02454*adc)"/>
</section>
<section name="MISC">
<define name="NOMINAL_AIRSPEED" value="15." unit="m/s"/>
<define name="CARROT" value="5." unit="s"/>
<define name="KILL_MODE_DISTANCE" value="(1.5*MAX_DIST_FROM_HOME)"/>
<define name="CONTROL_RATE" value="60" unit="Hz"/>
<!-- <define name="XBEE_INIT" value="\"ATPL2\rATRN1\rATTT80\r\""/> -->
<!-- <define name="NO_XBEE_API_INIT" value="TRUE"/> -->
<define name="ALT_KALMAN_ENABLED" value="FALSE"/>
<define name="TRIGGER_DELAY" value="1."/>
<define name="DEFAULT_CIRCLE_RADIUS" value="120."/>
<define name="MIN_CIRCLE_RADIUS" value="50."/>
</section>
<section name="VERTICAL CONTROL" prefix="V_CTL_">
<define name="POWER_CTL_BAT_NOMINAL" value="11.1" unit="volt"/>
<!-- outer loop proportional gain -->
<define name="ALTITUDE_PGAIN" value="-0.06"/> <!-- -0.024 -->
<!-- outer loop saturation -->
<define name="ALTITUDE_MAX_CLIMB" value="2."/>
<!-- auto throttle inner loop -->
<define name="AUTO_THROTTLE_NOMINAL_CRUISE_THROTTLE" value="0.45"/>
<define name="AUTO_THROTTLE_MIN_CRUISE_THROTTLE" value="0.35"/>
<define name="AUTO_THROTTLE_MAX_CRUISE_THROTTLE" value="0.85"/>
<define name="AUTO_THROTTLE_LOITER_TRIM" value="1000"/>
<define name="AUTO_THROTTLE_DASH_TRIM" value="-1200"/>
<define name="AUTO_THROTTLE_CLIMB_THROTTLE_INCREMENT" value="0.2" unit="%/(m/s)"/>
<define name="AUTO_THROTTLE_PGAIN" value="-0.023"/> <!-- -0.012 -->
<define name="AUTO_THROTTLE_IGAIN" value="0.01"/>
<define name="AUTO_THROTTLE_PITCH_OF_VZ_PGAIN" value="0.05"/>
<!-- auto pitch inner loop -->
<define name="AUTO_PITCH_PGAIN" value="-0.06"/> <!-- -0.03 -->
<define name="AUTO_PITCH_IGAIN" value="0.0"/>
<define name="AUTO_PITCH_MAX_PITCH" value="0.35"/>
<define name="AUTO_PITCH_MIN_PITCH" value="-0.35"/>
<define name="THROTTLE_SLEW" value="0.1"/>
</section>
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN" value="-0.9"/>
<define name="ROLL_MAX_SETPOINT" value="0.70" unit="radians"/> <!-- 0.5 -->
<define name="PITCH_MAX_SETPOINT" value="0.5" unit="radians"/>
<define name="PITCH_MIN_SETPOINT" value="-0.5" unit="radians"/>
<define name="ROLL_PGAIN" value="6600."/>
<define name="AILERON_OF_THROTTLE" value="0.0"/>
<define name="PITCH_PGAIN" value="-5500."/>
<define name="PITCH_DGAIN" value="0.4"/>
<define name="ELEVATOR_OF_ROLL" value="2400"/>
<!--define name="ROLL_ATTITUDE_GAIN" value="-7500"/>
<define name="ROLL_RATE_GAIN" value="-1500"/-->
</section>
<section name="NAV">
<define name="NAV_PITCH" value="0."/>
<define name="NAV_GLIDE_PITCH_TRIM" value="0"/>
</section>
<section name="AGGRESSIVE" prefix="AGR_">
<define name="BLEND_START" value="50"/><!-- Altitude Error to Initiate Aggressive Climb CANNOT BE ZERO!!-->
<define name="BLEND_END" value="15"/><!-- Altitude Error to Blend Aggressive to Regular Climb Modes CANNOT BE ZERO!!-->
<define name="CLIMB_THROTTLE" value="0.9"/><!-- Gaz for Aggressive Climb -->
<define name="CLIMB_PITCH" value="0.35"/><!-- Pitch for Aggressive Climb -->
<define name="DESCENT_THROTTLE" value="0.05"/><!-- Gaz for Aggressive Decent -->
<define name="DESCENT_PITCH" value="-0.35"/><!-- Pitch for Aggressive Decent -->
<define name="CLIMB_NAV_RATIO" value="0.8"/><!-- Percent Navigation for Altitude Error Equal to Start Altitude -->
<define name="DESCENT_NAV_RATIO" value="1.0"/>
</section>
<section name="FAILSAFE" prefix="FAILSAFE_">
<define name="DELAY_WITHOUT_GPS" value="2" unit="s"/>
<define name="DEFAULT_THROTTLE" value="0.3" unit="%"/>
<define name="DEFAULT_ROLL" value="0.3" unit="rad"/>
<define name="DEFAULT_PITCH" value="0.5" unit="rad"/>
<define name="HOME_RADIUS" value="100" unit="m"/>
</section>
<section name="DATALINK" prefix="DATALINK_">
<define name="DEVICE_TYPE" value="XBEE"/>
<define name="DEVICE_ADDRESS" value="...."/>
</section>
<section name="SIMU">
<define name="YAW_RESPONSE_FACTOR" value="0.5"/>
</section>
<section name="MICROMAG">
<define name="MM_SS_PIN" value="20"/>
<define name="MM_SS_IODIR" value="IO0DIR"/>
<define name="MM_SS_IOSET" value="IO0SET"/>
<define name="MM_SS_IOCLR" value="IO0CLR"/>
<define name="MM_RESET_PIN" value="29"/>
<define name="MM_RESET_IODIR" value="IO0DIR"/>
<define name="MM_RESET_IOSET" value="IO0SET"/>
<define name="MM_RESET_IOCLR" value="IO0CLR"/>
<define name="MM_DRDY_PINSEL" value="PINSEL1"/>
<define name="MM_DRDY_PINSEL_BIT" value="0"/>
<define name="MM_DRDY_PINSEL_VAL" value="1"/>
<define name="MM_DRDY_EINT" value="0"/>
<define name="MM_DRDY_VIC_IT" value="VIC_EINT0"/>
</section>
<makefile>
CONFIG = \"tiny_2_1.h\"
include $(PAPARAZZI_SRC)/conf/autopilot/tiny.makefile
FLASH_MODE=IAP
ap.CFLAGS += -DFBW -DAP -DBOARD_CONFIG=$(CONFIG) -DLED -DTIME_LED=1
ap.srcs = sys_time.c $(SRC_ARCH)/sys_time_hw.c $(SRC_ARCH)/armVIC.c main_fbw.c main_ap.c main.c
ap.srcs += commands.c
ap.CFLAGS += -DACTUATORS=\"servos_4017_hw.h\" -DSERVOS_4017
ap.srcs += $(SRC_ARCH)/servos_4017_hw.c actuators.c
ap.CFLAGS += -DRADIO_CONTROL
ap.srcs += radio_control.c $(SRC_ARCH)/ppm_hw.c
ap.CFLAGS += -DDOWNLINK -DUSE_UART1 -DDOWNLINK_TRANSPORT=XBeeTransport -DXBEE_UART=Uart1 -DDATALINK=XBEE -DUART1_BAUD=B57600
ap.srcs += downlink.c $(SRC_ARCH)/uart_hw.c datalink.c xbee.c
#TRANSPARENT
#ap.CFLAGS += -DDOWNLINK -DUSE_UART1 -DDOWNLINK_TRANSPORT=PprzTransport -DDOWNLINK_FBW_DEVICE=Uart1 -DDOWNLINK_AP_DEVICE=Uart1 -DPPRZ_UART=Uart1 -DDATALINK=PPRZ -DUART1_BAUD=B9600
#ap.srcs += downlink.c $(SRC_ARCH)/uart_hw.c datalink.c pprz_transport.c
ap.CFLAGS += -DINTER_MCU
ap.srcs += inter_mcu.c
ap.CFLAGS += -DADC -DUSE_ADC_0 -DUSE_ADC_1 -DUSE_ADC_2
ap.srcs += $(SRC_ARCH)/adc_hw.c
ap.CFLAGS += -DGPS -DUBX -DUSE_UART0 -DGPS_LINK=Uart0 -DUART0_BAUD=B38400 -DGPS_USE_LATLONG
# -DGPS_LED=2
ap.srcs += gps_ubx.c gps.c latlong.c
ap.CFLAGS += -DINFRARED -DALT_KALMAN -DWIND_INFO -DWIND_INFO_RET
ap.srcs += infrared.c estimator.c
ap.CFLAGS += -DNAV -DAGR_CLIMB -DLOITER_TRIM
ap.srcs += nav.c fw_h_ctl.c fw_v_ctl.c
ap.srcs += nav_line.c
ap.srcs += nav_survey_rectangle.c
ap.srcs += humid_sht.c
ap.CFLAGS += -DUSE_HUMID_SHT -DDAT_PIN=30 -DSCK_PIN=4
ap.CFLAGS += -DUSE_I2C0
ap.srcs += i2c.c $(SRC_ARCH)/i2c_hw.c
ap.CFLAGS += -DUSE_AIRSPEED_ETS
ap.srcs += airspeed_ets_o.c
ap.CFLAGS += -DUSE_IR_MLX
ap.srcs += ir_mlx.c
ap.CFLAGS += -DUSE_BARO_SCP
ap.srcs += baro_scp_i2c.c
ap.CFLAGS += -DMICROMAG_DRDY_VIC_SLOT=12 -DSSP_VIC_SLOT=11 -DUSE_MICROMAG_FW
ap.srcs += micromag_fw.c $(SRC_ARCH)/micromag_fw_hw.c
# Config for SITL simulation
include $(PAPARAZZI_SRC)/conf/autopilot/sitl.makefile
sim.CFLAGS += -DBOARD_CONFIG=\"tiny.h\" -DAGR_CLIMB -DLOITER_TRIM -DALT_KALMAN
sim.srcs += nav_line.c nav_survey_rectangle.c
</makefile>
</airframe>
+27 -3
View File
@@ -24,7 +24,10 @@
<define name="ALT_KALMAN"/>
<define name="WIND_INFO"/>
<define name="WIND_INFO_RET"/>
<define name="USE_I2C0"/>
<define name="SPI_MASTER"/>
<define name="USE_MICROMAG_FW"/>
<define name="MICROMAG_DRDY_VIC_SLOT" value="12"/>
<define name="SSP_VIC_SLOT" value="11"/>
</target>
<subsystem name="radio_control" type="ppm"/>
@@ -43,6 +46,7 @@
</subsystem>
<subsystem name="navigation"/>
<subsystem name="i2c"/>
<subsystem name="spi"/>
</firmware>
<firmware name="setup">
@@ -55,8 +59,9 @@
<!-- modules -->
<modules>
<load name="alt_srf08.xml"/>
<!--load name="baro_MS5534A.xml"/>
<load name="mag_micromag_fw.xml"/>
<!--load name="alt_srf08.xml"/>
<load name="baro_MS5534A.xml"/>
<load name="baro_bmp.xml"/>
<load name="baro_scp_i2c.xml"/>
<load name="light_temt.xml"/>
@@ -234,4 +239,23 @@
<define name="HOME_RADIUS" value="100" unit="m"/>
</section>
<section name="MICROMAG">
<define name="MM_SS_PIN" value="20"/>
<define name="MM_SS_IODIR" value="IO0DIR"/>
<define name="MM_SS_IOSET" value="IO0SET"/>
<define name="MM_SS_IOCLR" value="IO0CLR"/>
<define name="MM_RESET_PIN" value="29"/>
<define name="MM_RESET_IODIR" value="IO0DIR"/>
<define name="MM_RESET_IOSET" value="IO0SET"/>
<define name="MM_RESET_IOCLR" value="IO0CLR"/>
<define name="MM_DRDY_PINSEL" value="PINSEL1"/>
<define name="MM_DRDY_PINSEL_BIT" value="0"/>
<define name="MM_DRDY_PINSEL_VAL" value="1"/>
<define name="MM_DRDY_EINT" value="0"/>
<define name="MM_DRDY_VIC_IT" value="VIC_EINT0"/>
</section>
</airframe>
+16
View File
@@ -0,0 +1,16 @@
<!DOCTYPE module SYSTEM "module.dtd">
<module name="mag_micromag_fw" dir="meteo">
<header>
<file name="micromag_fw_hw.h"/>
<file name="micromag_fw.h"/>
</header>
<init fun="micromag_init()"/>
<periodic fun="micromag_periodic()" freq="60"/>
<event fun="micromag_event()"/>
<makefile>
<file_hw name="micromag_fw_hw.c"/>
<file name="micromag_fw.c"/>
</makefile>
</module>
@@ -7,13 +7,51 @@
*/
#include "led.h"
#include "micromag_fw.h"
#include "micromag_fw_hw.h"
#include "meteo/micromag_fw.h"
volatile uint8_t micromag_cur_axe;
static void SSP_ISR(void) __attribute__((naked));
static void EXTINT_ISR(void) __attribute__((naked));
static void SSP_ISR(void) {
ISR_ENTRY();
MmOnSpiIt();
VICVectAddr = 0x00000000; /* clear this interrupt from the VIC */
ISR_EXIT();
}
void EXTINT_ISR(void) {
ISR_ENTRY();
//LED_TOGGLE(3);
/* no, we won't do anything asynchronously, so just notify */
micromag_status = MM_GOT_EOC;
/* clear EINT */
SetBit(EXTINT,MM_DRDY_EINT);
// EXTINT = (1<<MM_DRDY_EINT);
VICVectAddr = 0x00000000; /* clear this interrupt from the VIC */
ISR_EXIT();
}
void micromag_hw_init( void ) {
/* setup pins for SSP (SCK, MISO, MOSI, SSEL) */
PINSEL1 |= SSP_PINSEL1_SCK | SSP_PINSEL1_MISO | SSP_PINSEL1_MOSI;
/* setup SSP */
SSPCR0 = SSPCR0_VAL;;
SSPCR1 = SSPCR1_VAL;
SSPCPSR = 0x02;
/* initialize interrupt vector */
VICIntSelect &= ~VIC_BIT( VIC_SPI1 ); /* SPI1 selected as IRQ */
VICIntEnable = VIC_BIT( VIC_SPI1 ); /* enable it */
_VIC_CNTL(SSP_VIC_SLOT) = VIC_ENABLE | VIC_SPI1;
_VIC_ADDR(SSP_VIC_SLOT) = (uint32_t)SSP_ISR; /* address of the ISR */
MmUnselect(); /* pin idles high */
/* configure SS pin */
@@ -37,16 +75,4 @@ void micromag_hw_init( void ) {
_VIC_ADDR(MICROMAG_DRDY_VIC_SLOT) = (uint32_t)EXTINT_ISR; // address of the ISR
}
void EXTINT_ISR(void) {
ISR_ENTRY();
//LED_TOGGLE(3);
/* no, we won't do anything asynchronously, so just notify */
micromag_status = MM_GOT_EOC;
/* clear EINT */
SetBit(EXTINT,MM_DRDY_EINT);
// EXTINT = (1<<MM_DRDY_EINT);
VICVectAddr = 0x00000000; /* clear this interrupt from the VIC */
ISR_EXIT();
}
@@ -88,6 +88,6 @@ extern volatile uint8_t micromag_cur_axe;
SpiEnableRti(); \
}
extern void micromag_hw_init( void );
#endif /* MICROMAG_HW_H */
-23
View File
@@ -95,10 +95,6 @@
#include "usb_serial.h"
#endif
#ifdef USE_MICROMAG_FW
#include "micromag_fw.h"
#endif
#ifdef USE_AIRSPEED_ETS
#include "airspeed_ets.h"
#endif // USE_AIRSPEED_ETS
@@ -497,10 +493,6 @@ void periodic_task_ap( void ) {
/* default: */
}
#ifdef USE_MICROMAG_FW
micromag_periodic();
#endif
#ifndef CONTROL_RATE
#define CONTROL_RATE 20
#endif
@@ -650,11 +642,6 @@ void init_ap( void ) {
#endif
nav_init();
#ifdef USE_MICROMAG_FW
micromag_init_ssp();
micromag_init();
#endif
modules_init();
/** - start interrupt task */
@@ -806,16 +793,6 @@ void event_task_ap( void ) {
}
#endif
#ifdef USE_MICROMAG_FW
if (micromag_status == MM_DATA_AVAILABLE) {
DOWNLINK_SEND_IMU_MAG_RAW(DefaultChannel,
&micromag_values[0],
&micromag_values[1],
&micromag_values[2] );
micromag_status = MM_IDLE;
}
#endif
if (inter_mcu_received_fbw) {
/* receive radio control task from fbw */
inter_mcu_received_fbw = FALSE;
-110
View File
@@ -1,110 +0,0 @@
#include "micromag_fw.h"
#include "led.h"
/* SSPCR0 settings */
#define SSP_DDS 0x07 << 0 /* data size : 8 bits */
#define SSP_FRF 0x00 << 4 /* frame format : SPI */
#define SSP_CPOL 0x00 << 6 /* clock polarity : data captured on first clock transition */
#define SSP_CPHA 0x00 << 7 /* clock phase : SCK idles low */
#define SSP_SCR 0x0F << 8 /* serial clock rate : divide by 16 */
/* SSPCR1 settings */
#define SSP_LBM 0x00 << 0 /* loopback mode : disabled */
#define SSP_SSE 0x00 << 1 /* SSP enable : disabled */
#define SSP_MS 0x00 << 2 /* master slave mode : master */
#define SSP_SOD 0x00 << 3 /* slave output disable : don't care when master */
#define SSPCR0_VAL (SSP_DDS | SSP_FRF | SSP_CPOL | SSP_CPHA | SSP_SCR )
#define SSPCR1_VAL (SSP_LBM | SSP_SSE | SSP_MS | SSP_SOD )
#define SSP_PINSEL1_SCK (2<<2)
#define SSP_PINSEL1_MISO (2<<4)
#define SSP_PINSEL1_MOSI (2<<6)
#define SSP_Enable() SetBit(SSPCR1, SSE);
#define SSP_Disable() ClearBit(SSPCR1, SSE);
#define SSP_EnableRxi() SetBit(SSPIMSC, RXIM)
#define SSP_DisableRxi() ClearBit(SSPIMSC, RXIM)
#define SSP_EnableTxi() SetBit(SSPIMSC, TXIM)
#define SSP_DisableTxi() ClearBit(SSPIMSC, TXIM)
#define SSP_EnableRti() SetBit(SSPIMSC, RTIM);
#define SSP_DisableRti() ClearBit(SSPIMSC, RTIM);
#define SSP_ClearRti() SetBit(SSPICR, RTIC);
volatile uint8_t micromag_status;
volatile int16_t micromag_values[MM_NB_AXIS];
static void SSP_ISR(void) __attribute__((naked));
void micromag_periodic( void ) {
static uint8_t cnt = 0;
if (micromag_status == MM_IDLE) {
// uint8_t * tab = &cnt;
// DOWNLINK_SEND_DEBUG(1,tab);
cnt = 0;
MmSendReq();
}
else if (micromag_status == MM_GOT_EOC) {
MmReadRes();
}
else if (micromag_status == MM_WAITING_EOC) {
cnt++;
if (cnt > 50) {cnt = 0; micromag_status = MM_IDLE;}
}
}
static void SSP_ISR(void) {
ISR_ENTRY();
MmOnSpiIt();
VICVectAddr = 0x00000000; /* clear this interrupt from the VIC */
ISR_EXIT();
}
void micromag_init_ssp(void) {
/* setup pins for SSP (SCK, MISO, MOSI, SSEL) */
PINSEL1 |= SSP_PINSEL1_SCK | SSP_PINSEL1_MISO | SSP_PINSEL1_MOSI;
/* setup SSP */
SSPCR0 = SSPCR0_VAL;;
SSPCR1 = SSPCR1_VAL;
SSPCPSR = 0x02;
/* initialize interrupt vector */
VICIntSelect &= ~VIC_BIT( VIC_SPI1 ); /* SPI1 selected as IRQ */
VICIntEnable = VIC_BIT( VIC_SPI1 ); /* enable it */
_VIC_CNTL(SSP_VIC_SLOT) = VIC_ENABLE | VIC_SPI1;
_VIC_ADDR(SSP_VIC_SLOT) = (uint32_t)SSP_ISR; /* address of the ISR */
}
void micromag_init( void ) {
micromag_hw_init();
uint8_t i;
for (i=0; i<MM_NB_AXIS; i++)
micromag_values[i] = 0;
micromag_status = MM_IDLE;
}
void micromag_reset() {
micromag_status = MM_IDLE;
}
void micromag_read() {
if (micromag_status == MM_IDLE) {
MmSendReq();
}
else if (micromag_status == MM_GOT_EOC) {
MmReadRes();
}
else if (micromag_status == MM_DATA_AVAILABLE) {
micromag_status == MM_IDLE;
}
}
+71
View File
@@ -0,0 +1,71 @@
#include "micromag_fw.h"
#include "meteo/micromag_fw_hw.h"
#include "led.h"
#include "uart.h"
#include "messages.h"
#include "downlink.h"
volatile uint8_t micromag_status;
volatile int16_t micromag_values[MM_NB_AXIS];
void micromag_periodic( void ) {
static uint8_t cnt = 0;
if (micromag_status == MM_IDLE) {
// uint8_t * tab = &cnt;
// DOWNLINK_SEND_DEBUG(1,tab);
cnt = 0;
MmSendReq();
}
else if (micromag_status == MM_GOT_EOC) {
MmReadRes();
}
else if (micromag_status == MM_WAITING_EOC) {
cnt++;
if (cnt > 50) {cnt = 0; micromag_status = MM_IDLE;}
}
}
void micromag_event( void ) {
int32_t mx=micromag_values[0];
int32_t my=micromag_values[1];
int32_t mz=micromag_values[2];
if (micromag_status == MM_DATA_AVAILABLE) {
DOWNLINK_SEND_IMU_MAG_RAW(DefaultChannel,
&mx,
&my,
&mz );
micromag_status = MM_IDLE;
}
}
void micromag_init( void ) {
micromag_hw_init();
uint8_t i;
for (i=0; i<MM_NB_AXIS; i++)
micromag_values[i] = 0;
micromag_status = MM_IDLE;
}
void micromag_reset() {
micromag_status = MM_IDLE;
}
void micromag_read() {
if (micromag_status == MM_IDLE) {
MmSendReq();
}
else if (micromag_status == MM_GOT_EOC) {
MmReadRes();
}
else if (micromag_status == MM_DATA_AVAILABLE) {
micromag_status == MM_IDLE;
}
}
@@ -5,12 +5,12 @@
#include "std.h"
#define MM_NB_AXIS 3
extern void micromag_init_ssp(void);
extern void micromag_init( void );
extern void micromag_read( void );
extern void micromag_reset( void);
extern void micromag_periodic( void );
extern void micromag_event( void );
#define MM_IDLE 0
#define MM_BUSY 1
@@ -41,13 +41,24 @@ extern void micromag_periodic( void );
#define SS_IOSET IO0SET
#define SS_IOCLR IO0CLR
#define SSPCR0_VAL (SSP_DDS | SSP_FRF | SSP_CPOL | SSP_CPHA | SSP_SCR )
#define SSPCR1_VAL (SSP_LBM | SSP_SSE | SSP_MS | SSP_SOD )
#define SSP_PINSEL1_SCK (2<<2)
#define SSP_PINSEL1_MISO (2<<4)
#define SSP_PINSEL1_MOSI (2<<6)
#define SSP_Enable() SetBit(SSPCR1, SSE);
#define SSP_Disable() ClearBit(SSPCR1, SSE);
#define SSP_EnableRxi() SetBit(SSPIMSC, RXIM)
#define SSP_DisableRxi() ClearBit(SSPIMSC, RXIM)
#define SSP_EnableTxi() SetBit(SSPIMSC, TXIM)
#define SSP_DisableTxi() ClearBit(SSPIMSC, TXIM)
#define SSP_EnableRti() SetBit(SSPIMSC, RTIM);
#define SSP_DisableRti() ClearBit(SSPIMSC, RTIM);
#define SSP_ClearRti() SetBit(SSPICR, RTIC);
extern volatile uint8_t micromag_status;
extern volatile int16_t micromag_values[MM_NB_AXIS];
extern void micromag_hw_init( void );
#include "micromag_fw_hw.h"
#endif /* MICROMAG_H */