|
| From: | Eduardo lavratti |
| Subject: | Re: [Paparazzi-devel] CHDK and digital_cam.xml |
| Date: | Mon, 28 May 2012 03:01:20 +0000 |
|
measure voltage on TPS PIN5 (input) when in SHOT and normal.
> Date: Sat, 26 May 2012 22:40:53 +0200 AGRESSiVA HiGH PERFORMANCE /// (o o) ____ooO__(_)__Ooo____ By Dudu > From: address@hidden > To: address@hidden > Subject: Re: [Paparazzi-devel] CHDK and digital_cam.xml > > The result: > Compiling OK > settings file: dc.xml > orange dots for autoshoots on GCS: OK > AUX voltage: low (constant 0.02V) > > :( > > Should I somehow enable this output? USE_LED or similar? > > Balazs > > > > > You might try that and tell me what you get : > > > > <modules> > > <load name="digital_cam.xml"> > > <define name="DC_SHUTTER_LED" value="6"/> > > <define name="LED_6_BANK" value="1"/> > > <define name="LED_6_PIN" value="18"/> > > <define name="PUSH" value="LED_ON" /> > > <define name="RELEASE" value="LED_OFF" /> > > </load> > > </modules> > > > > -----Message d'origine----- > > De : address@hidden > > [mailto:address@hidden De la > > part de address@hidden > > Envoyé : vendredi 25 mai 2012 22:13 > > À : address@hidden > > Objet : Re: [Paparazzi-devel] CHDK and digital_cam.xml > > > > Hi, > > > > I still didn't find the solution. It would mean big help for me, if > > someone could send me an airframe file with working AUX output. Or at > > least the relevant lines in it. > > > > Thx > > Balazs > > > >> Yes, I tried, but they seems already be defined. The compiler resulted > >> the warnings. I found similar lines in the tiny_2.11.h > >> > >> Balazs > >> > >> 2012.05.25. 8:05 keltezéssel, Cédric Marzer (privé) írta: > >>> Did you define the led pin and bank as in my airframe in a previous > >>> message ? > >>> > >>> *De :address@hidden > >>> [mailto:address@hidden *De la > >>> part > >>> de* Eduardo lavratti > >>> *Envoyé :* vendredi 25 mai 2012 02:26 *À :* Paparazzi developer forum > >>> *Objet :* Re: [Paparazzi-devel] CHDK and digital_cam.xml > >>> > >>> Balazs, you want AUX 5v because you like to use chdk remote shot ? > >>> you can use a simple transistor + 2 resistor to convert an 3.3v to 5v. > >>> > >>>> Date: Fri, 25 May 2012 00:14:17 +0200 > >>>> From: address@hidden <mailto:address@hidden> > >>>> To: address@hidden <mailto:address@hidden> > >>>> Subject: Re: [Paparazzi-devel] CHDK and digital_cam.xml > >>>> > >>>> Thx for the idea! Unfortunately it doesnt help to switch the power > >>>> on the AUX line. Meanwhile I checked that the CAM_SW output is > >>>> working correctly, it goes high (3.3V) periodicaly as it should in > >>>> autoshoot mode. > >>>> > >>>> But the AUX line is still down. I put only <define > >>>> name="POWER_SWITCH_LED"/> in the MISC section of the airframe file > >>>> but I still can't switch the power on with the power icon nor in > >>>> the settings tab provided by the switch.xml settings file. Although > >>>> I can see in the GCS, that the power_switch variable changes > >>>> according the commands, but the voltage at the AUX line is still > >>>> 0.3V. I even cheked the servo power voltage: the 5V rail seems to > >>>> be intact. > >>>> > >>>> Where should I look for errors, info or ideas? > >>>> > >>>> Some explanation: my Canon A800 can not be controlled with 3.3V of > >>>> the CAM_SW, therefore I would like to use the 5V of the AUX line to > >>>> shoot. > >>>> :( > >>>> > >>>> Balazs > >>>> > >>>> > >>>> > I think you need to define the pin and the bank of the led number > >>>> you > define as DC_SHUTTER_LED. > >>>> > I join my airframe file but it is not 100% mature ! Use at your > >>>> own > risk... > >>>> > > >>>> > > >>>> > > >>>> > On Wed, 2012-05-23 at 14:50 +0200, address@hidden > >>> <mailto:address@hidden>wrote: > >>>> >> Thank you Eduardo! > >>>> >> > >>>> >> My airframe file: > >>>> >> > >>>> >> > >>>> >> > >>>> >> <!DOCTYPE airframe SYSTEM "airframe.dtd"> >> >> <!-- > >>>> EasyGlider >> TWOGv1 >> Xsens MtiG >> AC4868 >> ETS Airspeed >> > >>>> >> --> >> >> <airframe name="Trainer60 - TWOG v1"> >> >> > >>>> <firmware name="fixedwing"> >> <target name="ap" board="twog_1.0"/> > >>>> >> <define name="AGR_CLIMB" /> >> <define name="USE_I2C0"/> >> > >>>> <define name="USE_AIRSPEED"/> >> <define name="USE_BARO_ETS"/> >> > >>>> <define name="USE_ADC"/> >> <define name="USE_ADC_3"/> <!-- accu > >>>> voltage--> >> <define name="USE_ADC_4"/> <!-- motor current--> >> > >>>> <define name="LOITER_TRIM" /> >> <define name="ALT_KALMAN" /> >> > >>>> <define name="ADC_CHANNEL_VSUPPLY" value="ADC_3"/> >> <subsystem > >>>> name="radio_control" type="ppm"/> >> <subsystem name="telemetry" > >>>> type="transparent"> >> <configure name="MODEM_BAUD" > >>>> value="B57600"/> >> </subsystem> >> <subsystem name="control"/> > >>>> >> <subsystem name="gps" type="xsens"/> >> <subsystem > >>>> name="navigation"/> >> <subsystem name="i2c"/> >> >> </firmware> > >>>> >> >> >> <!-- commands section --> >> <servos> >> <servo > >>>> name="AILERON" no="4" min="2000" neutral="1500" > >>>> >> max="1000"/> <!-- TWOG servo channel layout--> >> <servo > >>>> name="ELEVATOR" no="3" min="2000" neutral="1400" > >>>> >> max="1000"/> > >>>> >> <servo name="THROTTLE" no="7" min="1000" neutral="1000" > >>>> >> max="2000"/> > >>>> >> <servo name="RUDDER" no="6" min="1000" neutral="1500" > >>>> >> max="2000"/> > >>>> >> </servos> > >>>> >> > >>>> >> <!-- COMMANDS: generated by AP/RC --> >> <commands> >> <axis > >>>> name="THROTTLE" failsafe_value="0"/> >> <axis name="ROLL" > >>>> failsafe_value="0"/> >> <axis name="PITCH" failsafe_value="0"/> >> > >>>> <axis name="YAW" failsafe_value="0"/> >> <axis name="FLAPS" > >>>> failsafe_value="0"/> >> </commands> >> >> <!-- MANUAL MODE: links > >>>> the channels of the RC transmitter (defined >> in the Radio Control > >>>> file) >> to the commands defined above --> >> <rc_commands> >> > >>>> <set command="THROTTLE" value="@THROTTLE"/> >> <set command="ROLL" > >>>> value="@ROLL"/> >> <set command="PITCH" value="@PITCH"/> >> <set > >>>> command="YAW" value="@YAW"/> >> <set command="FLAPS" > >>>> value="@FLAPS"/> >> </rc_commands> >> >> <section name="MIXER"> > >>>> >> <define name="COMBI_SWITCH" value="0.4"/> <!--Orig: 1.0 --> >> > >>>> </section> >> >> <command_laws> >> <set servo="THROTTLE" > >>>> value="@THROTTLE"/> >> <set servo="ELEVATOR" value="@PITCH"/> >> > >>>> <set servo="RUDDER" value="@YAW + @ROLL*COMBI_SWITCH"/> >> <set > >>>> servo="AILERON" value="@ROLL"/> >> </command_laws> >> >> >> <!-- > >>>> AUTO1 MODE: max.pitch max.roll--> >> <section name="AUTO1" > >>>> prefix="AUTO1_"> >> <define name="MAX_ROLL" value="RadOfDeg(50)"/> > >>>> >> <define name="MAX_PITCH" value="RadOfDeg(40)"/> >> </section> > >>>> >> >> >> <!-- Battery --> >> <section name="BAT"> >> <define > >>>> name="ADC_CHANNEL_CURRENT" value="ADC_4"/> >> <define > >>>> name="MilliAmpereOfAdc(adc)" value="(100*adc)"/> >> <define > >>>> name="VOLTAGE_ADC_A" value="0.05"/> >> <define name="VOLTAGE_ADC_B" > >>>> value="1"/> >> <define name="VoltageOfAdc(adc)" value > >>>> ="(VOLTAGE_ADC_A * adc + >> VOLTAGE_ADC_B)"/> >> <define > >>>> name="CATASTROPHIC_BAT_LEVEL" value="19.0" unit="V"/> >> <define > >>>> name="CRITIC_BAT_LEVEL" value="20.0" unit="V"/> >> <define > >>>> name="LOW_BAT_LEVEL" value="21.0" unit="V"/> >> <define > >>>> name="MAX_BAT_LEVEL" value="25.0" unit="V"/> >> </section> >> >> > >>>> <!-- Horizontal control --> >> <section name="HORIZONTAL CONTROL" > >>>> prefix="H_CTL_"> >> <define name="COURSE_PGAIN" value="-0.7"/> <!-- > >>>> course error-> roll >> command orig: -1.0--> >> <define > >>>> name="ROLL_MAX_SETPOINT" value="0.7" unit="radians"/> <!-- >> max. > >>>> roll command --> >> <define name="ROLL_SLEW" value="0.1"/> <!-- >> > >>>> roll rate--> >> <define name="ROLL_ATTITUDE_GAIN" value="-9000"/> > >>>> <!-- >> roll command from roll error--> >> <define > >>>> name="ROLL_RATE_GAIN" value="-1500"/> <!-- >> if gyro is > >>>> installed--> >> <define name="PITCH_DGAIN" value="1.5"/> >> > >>>> <define name="PITCH_PGAIN" value="-7000"/> >> <define > >>>> name="ELEVATOR_OF_ROLL" value="1700"/> <!-- >> orig 1300 --> >> > >>>> <define name="PITCH_MAX_SETPOINT" value="0.5" unit="radians"/> >> > >>>> <define name="PITCH_MIN_SETPOINT" value="-0.25" unit="radians"/> >> > >>>> >> </section> >> >> <!-- Vertical control --> >> <section > >>>> name="VERTICAL CONTROL" prefix="V_CTL_"> >> <define > >>>> name="ALTITUDE_PGAIN" value="-0.1" unit="(m/s)/m"/> <!-- >> > >>>> altitude error->rate of climb --> >> <define > >>>> name="ALTITUDE_MAX_CLIMB" value="1" unit="m/s"/> <!-- >> max. rate > >>>> of climb --> >> <!-- auto throttle inner loop --> >> <define > >>>> name="AUTO_THROTTLE_NOMINAL_CRUISE_THROTTLE" value="0.6" > >>>> >> unit="%"/> > >>>> >> <define name="AUTO_THROTTLE_MIN_CRUISE_THROTTLE" value="0.2" > >>>> >> unit="%"/> > >>>> >> <define name="AUTO_THROTTLE_MAX_CRUISE_THROTTLE" value="1.0" > >>>> >> unit="%"/> > >>>> >> <define name="AUTO_THROTTLE_LOITER_TRIM" value="1500" > >>>> >> unit="pprz_t"/> > >>>> >> <define name="AUTO_THROTTLE_DASH_TRIM" value="-4000" > >>>> unit="pprz_t"/> > >>>> >> <define name="AUTO_THROTTLE_CLIMB_THROTTLE_INCREMENT" value="0.3" > >>>> >> unit="%/(m/s)"/> > >>>> >> <define name="AUTO_THROTTLE_PGAIN" value="-0.008" > >>>> unit="%/(m/s)"/> >> <define name="AUTO_THROTTLE_IGAIN" > >>>> value="0.1"/> >> <define name="AUTO_THROTTLE_PITCH_OF_VZ_PGAIN" > >>>> value="0.1" > >>>> >> unit="rad/(m/s)"/> <!-- orig 0.05 --> >> <!-- auto pitch inner > >>>> loop --> >> <define name="AUTO_PITCH_PGAIN" value="-0.2"/> <!-- > >>>> orig 0.1 --> >> <define name="AUTO_PITCH_IGAIN" value="0.025"/> >> > >>>> <define name="AUTO_PITCH_MAX_PITCH" value="0.5"/> >> <define > >>>> name="AUTO_PITCH_MIN_PITCH" value="-0.5"/> >> <define > >>>> name="THROTTLE_SLEW_LIMITER" value="2" unit="s"/> >> <!-- auto > >>>> airspeed and altitude inner loop --> >> <define > >>>> name="AUTO_AIRSPEED_SETPOINT" value="11.0" unit="m/s"/> >> <!--orig > >>>> 10.5 --> >> <define name="AUTO_AIRSPEED_PGAIN" value="0.060"/> <!-- > >>>> orig 0.060 >> --> >> <define name="AUTO_AIRSPEED_IGAIN" > >>>> value="0.050"/> <!-- orig >> 0.050 --> >> <define > >>>> name="AUTO_GROUNDSPEED_SETPOINT" value="7.0" unit="m/s"/> >> > >>>> <define name="AUTO_GROUNDSPEED_PGAIN" value="0.75"/> >> <define > >>>> name="AUTO_GROUNDSPEED_IGAIN" value="0.25"/> >> </section> >> >> > >>>> <section name="MISC"> >> <define name="NOMINAL_AIRSPEED" > >>>> value="14.0" unit="m/s"/> >> <!--mainly for simulator --> >> > >>>> <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="DEFAULT_CIRCLE_RADIUS" value="120."/> >> <define > >>>> name="UNLOCKED_HOME_MODE" value="FALSE"/> <!-- if true, >> HOME > >>>> mode does not get stuck --> >> <define name="RC_LOST_MODE" > >>>> value="PPRZ_MODE_AUTO2"/> >> <define name="ALT_KALMAN_ENABLED" > >>>> value="TRUE"/> >> >> <!-- >> <define name="GLIDE_AIRSPEED" > >>>> value="10"/> >> <define name="GLIDE_VSPEED" value="3."/> >> > >>>> <define name="GLIDE_PITCH" value="45" unit="deg"/> >> --> >> > >>>> </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="20"/><!-- Altitude Error to >> > >>>> Initiate Aggressive Climb CANNOT BE ZERO!!--> >> <define > >>>> name="BLEND_END" value="10"/><!-- Altitude Error to Blend >> > >>>> Aggressive to Regular Climb Modes CANNOT BE ZERO!!--> >> <define > >>>> name="CLIMB_THROTTLE" value="1.00"/><!-- Gaz for Aggressive >> > >>>> Climb --> >> <define name="CLIMB_PITCH" value="0.5"/><!-- Pitch for > >>>> Aggressive >> Climb --> >> <define name="DESCENT_THROTTLE" > >>>> value="0.1"/><!-- Gaz for Aggressive >> Decent --> >> <define > >>>> name="DESCENT_PITCH" value="-0.25"/><!-- 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="5" unit="s"/> >> <define > >>>> name="DEFAULT_THROTTLE" value="0.3" unit="%"/> >> <define > >>>> name="DEFAULT_ROLL" value="0.3" unit="rad"/> >> <define > >>>> name="DEFAULT_PITCH" value="0.3" unit="rad"/> >> </section> >> >> > >>>> <!-- <section name="DATALINK" prefix="DATALINK_"> >> <define > >>>> name="DEVICE_TYPE" value="PPRZ"/> >> <define name="DEVICE_ADDRESS" > >>>> value="...."/> >> </section> --> >> >> >> <section name="XSENS"> > >>>> >> <!-- <define name="GPS_IMU_LEVER_ARM_X" value="-0.285f"/> --> >> > >>>> <!-- <define name="GPS_IMU_LEVER_ARM_Y" value="0.0f"/> --> >> <!-- > >>>> <define name="GPS_IMU_LEVER_ARM_Z" value="0.0f"/> --> >> <define > >>>> name="INS_PITCH_NEUTRAL_DEFAULT" value="0.0f"/> >> <define > >>>> name="INS_ROLL_NEUTRAL_DEFAULT" value="0.0f"/> >> </section> >> > >>>> >> <section name="DIGITAL_CAMERA" prefix="DC_"> >> <define > >>>> name="AUTOSHOOT_QUARTERSEC_PERIOD" value="6" > >>>> >> unit="quarter_second"/> > >>>> >> <define name="AUTOSHOOT_METER_GRID" value="50" unit="meter"/> > >>>> >> </section> >> >> <modules> >> <load > >>>> name="ins_xsens_MTiG_fixedwing.xml"> > >>>> >> <configure name="XSENS_UART_NR" value="0"/> >> <define > >>>> name="XSENS_BACKWARDS" /> >> </load> >> <load > >>>> name="airspeed_ets.xml"> >> <define name="AIRSPEED_ETS_SCALE" > >>>> value="1.8"/> >> <define name="AIRSPEED_ETS_OFFSET" value="4"/> >> > >>>> <define name="AIRSPEED_ETS_I2C_DEV" value="i2c0"/> >> <!-- <define > >>>> name="SENSOR_SYNC_SEND"/> Sending the raw airspeed >> by telemetry > >>>> (high bandwith)--> >> </load> >> <load name="baro_ets.xml"> >> > >>>> <define name="BARO_ETS_TELEMETRY"/> <!-- Sending the barometric >> > >>>> pressure by telemetry --> >> </load> >> <load > >>>> name="digital_cam.xml" > >> <define name="DC_SHUTTER_LED" > >>>> value="5"/> >> <define name="POWER_SWITCH_LED" value="4"/> >> > >>>> </load> >> <!--<load name="adc_generic.xml"> --> >> <!-- > >>>> <configure name="ADC_CHANNEL_GENERIC1" value="ADC_3"/> --> >> <!-- > >>>> <configure name="ADC_CHANNEL_GENERIC2" value="ADC_4"/> --> >> > >>>> <!--</load> --> >> </modules> >> >> >> >> >> </airframe> >> > >>>> >> >> >> >> >> >> >> > >>>> _______________________________________________ > >>>> >> Paparazzi-devel mailing list > >>>> >> address@hidden <mailto:address@hidden> > >>>> >> https://lists.nongnu.org/mailman/listinfo/paparazzi-devel > >>>> > > >>>> > _______________________________________________ > >>>> > Paparazzi-devel mailing list > >>>> > address@hidden <mailto:address@hidden> > >>>> > https://lists.nongnu.org/mailman/listinfo/paparazzi-devel > >>>> > > >>>> > >>>> > >>>> > >>>> _______________________________________________ > >>>> Paparazzi-devel mailing list > >>>> address@hidden <mailto:address@hidden> > >>>> https://lists.nongnu.org/mailman/listinfo/paparazzi-devel > >>> > >>> > >>> > >>> _______________________________________________ > >>> Paparazzi-devel mailing list > >>> address@hidden > >>> https://lists.nongnu.org/mailman/listinfo/paparazzi-devel > >> > >> -- > >> Balazs GATI, PhD > >> Department of Aircraft and Ships > >> Budapest University of Technology and Economics > >> > >> Address: Budapest > >> Stoczek u 6. J. ép. 423 > >> 1111 > >> Tel: +(36)-1-463-1960 > >> Fax: +(36)-1-463-3080 > >> Homepage: http://rht.bme.hu/~gatib/ > >> > >> _______________________________________________ > >> Paparazzi-devel mailing list > >> address@hidden > >> https://lists.nongnu.org/mailman/listinfo/paparazzi-devel > >> > > > > > > > > _______________________________________________ > > Paparazzi-devel mailing list > > address@hidden > > https://lists.nongnu.org/mailman/listinfo/paparazzi-devel > > > > > > > > _______________________________________________ > > Paparazzi-devel mailing list > > address@hidden > > https://lists.nongnu.org/mailman/listinfo/paparazzi-devel > > > > > > _______________________________________________ > Paparazzi-devel mailing list > address@hidden > https://lists.nongnu.org/mailman/listinfo/paparazzi-devel |
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