Hi,
i made same test with die discoveryF4.
In actually master and stabile version of paparazzi the measurement
of the bat voltage is not working.
In a master version from 11.2013 656a13 -v5.1 its runs perfect.
Can some test it in the stabile Version 5.2 and 5.0?
Regards
Heinrich
<!DOCTYPE
airframe SYSTEM "../airframe.dtd">
<!-- Discovery F4
for normal plane, with DROTEK 10Dof IMU -->
<airframe
name="HB_DiscoveryFixed">
<firmware
name="fixedwing">
<target
name="ap"
board="stm32f4_discovery"/>
<target name="sim" board="pc"/>
<!--#######################################################################################-->
<!--############################## GLOBAL
DEFINITIONS
#################################-->
<!--#######################################################################################-->
<!--
"configure" pass the definition in the makefile -->
<configure
name="SYS_TIME_LED" value="3"/>
<!--
"define" pass the definition in the C preprocessor
-->
<define
name="USE_LED_3"/>
<define
name="USE_LED_4"/>
<define
name="USE_LED_5"/>
<define
name="USE_LED_6"/>
<define name="USE_ADC_1" value="1"/>
<define name="USE_ADC_2"
value="1"/>
<define name="USE_ADC_3" value="1"/>
<define name="USE_ADC_4"
value="1"/>
<define name="AGR_CLIMB"/>
<define name="WIND_INFO"/>
<define
name="WIND_INFO_RET"/>
<define
name="STRONG_WIND"/>
<define
name="ALT_KALMAN"/>
<define
name="USE_I2C"/>
<define
name="USE_I2C2"/>
<!-- <define
name="SENSOR_SYNC_SEND"/>
-->
<define
name="USE_AHRS_GPS_ACCELERATIONS"/>
<define
name="USE_GROUNDSPEED_CONTROL"/>
<configure
name="PERIODIC_FREQUENCY" value="120"/>
<configure
name="AHRS_PROPAGATE_FREQUENCY" value="100"/>
<configure
name="AHRS_CORRECT_FREQUENCY" value="100"/>
<!-- <define
name="ADC_CHANNEL_VSUPPLY"
value="ADC_1" />
-->
<!-- <define
name="MEASURE_AIRSPEED"/>
-->
<!-- <define
name="USE_AIRSPEED"/>
-->
<!-- <define
name="USE_BAROMETER"/>
-->
<!-- <define
name="USE_INS_NAV_INIT" value=FALSE"/> --> <!--Set Home
to flight plan coordinates -->
<!--#######################################################################################-->
<!--############################## SUBSYSTEMS #################################-->
<!--#######################################################################################-->
<!--
"define" goes to the C preprocessor, "configure" configures
the makefile -->
<subsystem
name="telemetry" type="transparent">
<configure name="MODEM_BAUD"
value="B57600"/>
<configure
name="MODEM_PORT" value="UART2"/>
<!-- <configure
name="MODEM_LED"
value="5"/>
-->
</subsystem>
<subsystem name="gps" type="ublox">
<configure
name="GPS_BAUD"
value="B38400"/>
<configure
name="GPS_PORT"
value="UART3"/>
<configure
name="GPS_LED" value="6"/>
<!-- <configure
name="GPS_LED"
value="none"/> -->
</subsystem>
<subsystem
name="control" />
<subsystem
name="radio_control" type="ppm"/>
<subsystem name="navigation"
type="extra"/>
<!--
subsystems/imu/imu_drotek_10dof_v2.c:42:1:
note: #pragma message: Config: Gyro/Accel output rate is 100Hz
subsystems/imu/imu_drotek_10dof_v2.c:44:1:
note: #pragma message: Config: DROTEK_2_SMPLRT_DIV = 9
subsystems/imu/imu_drotek_10dof_v2.c:45:1:
note: #pragma message: Config: DROTEK_2_LOWPASS_FILTER =
MPU60X0_DLPF_42HZ
subsystems/imu/imu_drotek_10dof_v2.c:50:1: note: #pragma
message: Config: DROTEK_2_GYRO_RANGE = MPU60X0_GYRO_RANGE_1000
subsystems/imu/imu_drotek_10dof_v2.c:55:1:
note: #pragma message: Config: DROTEK_2_ACCEL_RANGE =
MPU60X0_ACCEL_RANGE_8G
subsystems/imu/imu_drotek_10dof_v2.c:60:1:
note: #pragma message: Config: DROTEK_2_MPU_I2C_ADDR = 0xD2
subsystems/imu/imu_drotek_10dof_v2.c:65:1:
note: #pragma message: Config: DROTEK_2_HMC_I2C_ADDR = 0x3C
-->
<subsystem
name="imu" type="drotek_10dof_v2">
<define
name="DROTEK_2_MPU_I2C_ADDR" value="MPU60X0_ADDR_ALT"
/>
<!--
<define
name="IMU_DROTEK_2_ORIENTATION_IC_UP" value="1" />
-->
</subsystem>
<!-- MAGNETOMETER IS NOT WORKING IN DCM
BE CAREFULL -->
<!--
olri <subsystem name="ahrs" type="float_dcm">
-->
<subsystem
name="ahrs" type="int_cmpl_quat">
<define
name="USE_MAGNETOMETER" value="1"/>
<define
name="USE_MAGNETOMETER_ONGROUND" value="0"/>
</subsystem>
<subsystem name="ins"
type="alt_float"/>
<!-- <subsystem
name="spi" type="master"/> -->
</firmware>
<!--#######################################################################################-->
<!--################################ MODULES #################################-->
<!--#######################################################################################-->
<modules>
<!-- baro_ms5611_i2c Alternate
address -->
<load
name="baro_ms5611_i2c.xml">
<define
name="MS5611_I2C_DEV"
value="i2c2" />
<define
name="MS5611_SLAVE_ADDR=0xEE"/>
<define
name="MS5611_SEND_BARO_ALTITUDE"/>
<!-- olri
<define
name="SENSOR_SYNC_SEND"/>
olri -->
</load>
<load
name="gps_ubx_ucenter.xml"/>
</modules>
<!--#######################################################################################-->
<!--############################# SERVOS
AND CONTROLS
#################################-->
<!--#######################################################################################-->
<!--
commands section -->
<servos>
<servo name="AILERON"
no="0"
min="988" neutral="1500"
max="2012"/>
<servo
name="ELEVATOR" no="1"
min="988" neutral="1500"
max="2012"/>
<servo
name="ENGINE" no="2"
min="1060" neutral="1060"
max="2012"/>
<servo
name="FLAPS" no="3"
min="988" neutral="988" max="2012"/>
<servo name="ANT_PAN"
no="4"
min="950" neutral="1485"
max="2050"/>
<servo
name="CAM_ZOOM" no="5"
min="998" neutral="1500"
max="2012"/>
<servo
name="CAM_PAN" no="6"
min="970" neutral="1500"
max="2075"/>
<servo
name="CAM_TILT" no="7"
min="1040" neutral="1500"
max="1900"/>
</servos>
<commands>
<axis name="ROLL" failsafe_value="0"/>
<axis name="PITCH" failsafe_value="0"/>
<axis name="THROTTLE" failsafe_value="0"/>
<axis name="FLAPS" failsafe_value="0"/>
<axis name="ANT_PAN" failsafe_value="0"/>
<axis name="CAM_ZOOM" failsafe_value="0"/>
<axis name="CAM_PAN" failsafe_value="0"/>
<axis name="CAM_TILT" failsafe_value="0"/>
</commands>
<rc_commands>
<set command="ROLL"
value="@ROLL"/>
<set command="PITCH"
value="@PITCH"/>
<set command="THROTTLE"
value="@THROTTLE"/>
<set command="FLAPS" value="@FLAPS"/>
</rc_commands>
<section name="MIXER">
<define
name="FLAP_TO_ELEVATOR_MIX" value="-0.15"/>
</section>
<command_laws>
<let var="elevator" value="(@PITCH
+ (@FLAPS *
FLAP_TO_ELEVATOR_MIX))"/>
<set servo="ENGINE" value="@THROTTLE"/>
<set servo="AILERON" value="@ROLL"/>
<set servo="ELEVATOR" value="$elevator"/>
<set servo="ANT_PAN" value="@ANT_PAN"/>
<set servo="FLAPS"
value="@FLAPS"/>
<set servo="CAM_ZOOM" value="@CAM_ZOOM"/>
<set servo="CAM_PAN" value="@CAM_PAN"/>
<set servo="CAM_TILT" value="@CAM_TILT"/>
</command_laws>
<!--
EMPTY "auto_rc_commands" block means NO RC RUDDER CONTROL IN AUTO2
AND AUTO1 -->
<auto_rc_commands>
<!-- <set command="YAW" value="@YAW"/>
-->
</auto_rc_commands>
<ap_only_commands>
<copy
command="ANT_PAN"/>
</ap_only_commands>
<!--#######################################################################################-->
<!--################################# I M
U SETUP #################################-->
<!--#######################################################################################-->
<!--
Normalized Local magnetic field obtained from
http://www.ngdc.noaa.gov/geomag-web/#igrfwmm
-->
<!-- Magnetic field intensity / total field strength
-->
<!-- Calculated for PIRAEUS HELLAS 31 MAY 2013 declination =
3.59 degrees, 5.9 deg/year-->
<section name="AHRS"
prefix="AHRS_" >
<define name="H_X" value="(26536.9/45821.6)"
/>
<define
name="H_Y" value="(1850.1/45821.6)" />
<define name="H_Z"
value="(37309.3/45821.6) " />
<define name="MAG_DECLINATION"
value="(RadOfDeg(4))" />
</section>
<section
name="IMU" prefix="IMU_">
<define name="GYRO_P_SIGN" value="1"/>
<define name="GYRO_Q_SIGN"
value="1"/>
<define name="GYRO_R_SIGN" value="1"/>
<define name="ACCEL_X_SIGN"
value="1"/>
<define name="ACCEL_Y_SIGN" value="1"/>
<define name="ACCEL_Z_SIGN"
value="1"/>
<define name="MAG_X_SIGN"
value="1"/>
<define name="MAG_Y_SIGN" value="1"/>
<define name="MAG_Z_SIGN"
value="1"/>
<define name="GYRO_P_Q" value="0."/>
<define name="GYRO_P_R"
value="0."/>
<define name="GYRO_Q_P" value="0."/>
<define name="GYRO_Q_R"
value="0."/>
<define name="GYRO_R_P" value="0."/>
<define name="GYRO_R_Q"
value="0."/>
<!-- Found with calibrate.py script and visual observation of
the RAW
values -->
<!--
<define name="ACCEL_X_NEUTRAL"
value="-223"/>
<define name="ACCEL_Y_NEUTRAL"
value="-704"/>
<define name="ACCEL_Z_NEUTRAL"
value="-40"/>
-->
<define
name="GYRO_P_NEUTRAL" value="5" />
<define name="GYRO_Q_NEUTRAL"
value="25" />
<define name="GYRO_R_NEUTRAL" value="12"
/>
<!-- SENS = 2048 LSB/g / 9.81 ms2/g = 208.766564729 LSB/ms2
/ 10bit FRAC: 1024 / 208.7665 -->
<!-- Found with calibrate.py script -->
<define
name="ACCEL_X_NEUTRAL" value="8"/>
<define
name="ACCEL_Y_NEUTRAL" value="25"/>
<define
name="ACCEL_Z_NEUTRAL" value="-55"/>
<define name="ACCEL_X_SENS"
value="2.46169818688" integer="16"/>
<define name="ACCEL_Y_SENS"
value="2.4400141151" integer="16"/>
<define name="ACCEL_Z_SENS"
value="2.42446843209" integer="16"/>
<define
name="BODY_TO_IMU_PHI"
value="9.7" unit="deg"/>
<define
name="BODY_TO_IMU_THETA" value="-2.4"
unit="deg"/>
<define name="BODY_TO_IMU_PSI" value="0."
unit="deg"/>
<!-- Found with calibrate.py script
-->
<define
name="MAG_X_NEUTRAL" value="73"/>
<define name="MAG_Y_NEUTRAL"
value="118"/>
<define name="MAG_Z_NEUTRAL"
value="169"/>
<define name="MAG_X_SENS" value="4.25741044617"
integer="16"/>
<define name="MAG_Y_SENS" value="4.26451705702"
integer="16"/>
<define name="MAG_Z_SENS" value="4.87790997442"
integer="16"/>
</section>
<!--#######################################################################################-->
<!--################## AIRCRAFT ATTITUDE
TRIMMING AND AUTO1
LIMITS
#####################-->
<!--#######################################################################################-->
<section
name="INS" prefix="INS_">
<define name="ROLL_NEUTRAL_DEFAULT"
value="RadOfDeg(0.)" unit="radians"/>
<define
name="PITCH_NEUTRAL_DEFAULT" value="RadOfDeg(0.)"
unit="radians"/>
</section>
<section
name="AUTO1" prefix="AUTO1_">
<define name="MAX_ROLL"
value="40" unit="deg"/>
<define name="MAX_PITCH" value="30"
unit="deg"/>
</section>
<!--#######################################################################################-->
<!--######################### AIRCRAFT
VERTICAL CONTROL SETUP
########################-->
<!--#######################################################################################-->
<section
name="VERTICAL CONTROL" prefix="V_CTL_">
<!-- OUTER LOOP
PARAMETERS -->
<!-- The
below definition affect the throttle percentage shown on the GCS. -->
<define
name="POWER_CTL_BAT_NOMINAL" value="12.6"
unit="volt"/>
<!-- outer loop ALTITUDE proportional gain -->
<define name="ALTITUDE_PGAIN"
value="0.07" unit="(m/s)/m"/>
<!-- outer loop ALTITUDE LIMIT
(saturation) -->
<define
name="ALTITUDE_MAX_CLIMB" value="3"
unit="m/s"/>
<!-- outer loop AIRSPEED proportional gain -->
<define name="AIRSPEED_PGAIN" value="0.2"/>
<!-- INNER LOOP
PARAMETERS -->
<!--
The below definitions are used almost always -->
<define
name="AUTO_THROTTLE_NOMINAL_CRUISE_THROTTLE" value="0.50"
unit="%"/>
<define
name="AUTO_THROTTLE_MIN_CRUISE_THROTTLE" value="0.40"
unit="%"/>
<define
name="AUTO_THROTTLE_MAX_CRUISE_THROTTLE" value="0.70"
unit="%"/>
<define
name="THROTTLE_SLEW_LIMITER" value="0.6"
unit="s"/>
<define
name="AUTO_PITCH_MAX_PITCH" value="RadOfDeg(20)"/>
<define
name="AUTO_PITCH_MIN_PITCH" value="RadOfDeg(-20)"/>
<!--
Climb loop (throttle) -->
<define
name="AUTO_THROTTLE_CLIMB_THROTTLE_INCREMENT" value="0.1"
unit="%/(m/s)"/>
<define
name="AUTO_THROTTLE_NOMINAL_CRUISE_PITCH" value="0.0"
unit="rad"/>
<define
name="AUTO_THROTTLE_PGAIN" value="0.008"unit="%/(m/s)"/>
<define
name="AUTO_THROTTLE_IGAIN" value="0.0"/>
<define
name="AUTO_THROTTLE_DGAIN" value="0.001"/>
<!-- Climb loop (pitch) -->
<!-- magnitude of elevator movement
on altitude change -->
<define
name="AUTO_THROTTLE_PITCH_OF_VZ_PGAIN" value="0.15"
unit="rad/(m/s)"/> <!-- 0.05 -->
<define
name="AUTO_PITCH_PGAIN"
value="0.04"/>
<!--0.052-->
<define name="AUTO_PITCH_DGAIN" value="0.0"/>
<define
name="AUTO_PITCH_IGAIN"
value="0.01"/>
<!--0.065-->
<!--
Loiter and Dash trimming -->
<define
name="AUTO_THROTTLE_LOITER_TRIM" value="0"
unit="pprz_t"/>
<define
name="AUTO_THROTTLE_DASH_TRIM" value="0"
unit="pprz_t"/>
<define
name="PITCH_LOITER_TRIM" value="0"
unit="pprz_t"/>
<define
name="PITCH_DASH_TRIM"
value="0"
unit="pprz_t"/>
<!-- The below definitions are used for the "energy"
control loop -->
<define
name="AUTO_THROTTLE_OF_AIRSPEED_PGAIN" value="0"
/>
<define
name="AUTO_THROTTLE_OF_AIRSPEED_IGAIN" value="0.01"
/>
<define
name="AUTO_PITCH_OF_AIRSPEED_PGAIN" value="0" />
<define
name="AUTO_PITCH_OF_AIRSPEED_IGAIN" value="0" />
<define
name="AUTO_PITCH_OF_AIRSPEED_DGAIN" value="0" />
<define
name="ENERGY_TOT_PGAIN"
value="0.35"
/>
<define
name="ENERGY_TOT_IGAIN"
value="0.25"
/>
<define
name="ENERGY_DIFF_PGAIN" value="0.30" />
<define
name="ENERGY_DIFF_IGAIN" value="0.20" />
<define
name="DESIRED_ACCELERATION" value="0.3" />
<define
name="MAX_ACCELERATION"
value="0.5"
/>
<define
name="AUTO_AIRSPEED_SETPOINT" value="15."
unit="m/s"/>
<define
name="AUTO_GROUNDSPEED_SETPOINT" value="15."
unit="m/s"/>
<define
name="AUTO_GROUNDSPEED_PGAIN" value="0."/>
<define
name="AUTO_GROUNDSPEED_IGAIN" value="0"/>
</section>
<!--#######################################################################################-->
<!--######################## AIRCRAFT
HORIZONTAL CONTROL SETUP ########################-->
<!--#######################################################################################-->
<section
name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN"
value="0.8"/>
<!-- <define
name="COURSE_DGAIN"
value="0.8"/>
-->
<define
name="COURSE_PRE_BANK_CORRECTION" value="1."/>
<define
name="PITCH_MAX_SETPOINT" value="20"
unit="deg"/>
<define
name="PITCH_MIN_SETPOINT" value="-20"
unit="deg"/>
<define
name="PITCH_PGAIN"
value="8000."/>
<!-- The below two definitions only for
stabilization adaptive -->
<define
name="PITCH_DGAIN"
value="6."/>
<define name="PITCH_IGAIN"
value="100."/>
<define
name="ROLL_MAX_SETPOINT" value="30"
unit="deg"/>
<define
name="ROLL_SLEW" value="0.1"/>
<define
name="ROLL_ATTITUDE_GAIN" value="8000"/>
<define name="ROLL_RATE_GAIN"
value="500."/>
<define name="PITCH_OF_ROLL"
value="RadOfDeg(1.0)"/>
<define
name="ELEVATOR_OF_ROLL"
value="1000"/>
<define
name="AILERON_OF_THROTTLE" value="0.0"/>
<!-- The below definitions are used
only for stabilization adaptive -->
<define
name="PITCH_DGAIN"
value="6."/>
<define name="PITCH_IGAIN"
value="100."/>
<define name="ROLL_KFFA"
value="0"/>
<define name="ROLL_KFFD"
value="0"/>
<define name="PITCH_KFFA"
value="0."/>
<define name="PITCH_KFFD"
value="0."/>
</section>
<!--#######################################################################################-->
<!--############################ AIRBORNE
BATTERY SETUP #############################-->
<!--#######################################################################################-->
<section
name="BAT">
<define
name="MILLIAMP_AT_FULL_THROTTLE" value="5000"/>
<define name="BAT_CAPACITY"
value="10000."/>
<define
name="FUEL_RESERVE_SECONDS" value="300"
unit="s"/>
<define
name="CATASTROPHIC_BAT_LEVEL" value="8"
unit="V"/>
<define
name="CRITIC_BAT_LEVEL"
value="9.3"
unit="V"/>
<define
name="LOW_BAT_LEVEL"
value="10.5"
unit="V"/>
<define
name="MAX_BAT_LEVEL"
value="12.6"
unit="V"/>
<define name="VOLTAGE_ADC_SCALE"
value="0.018864469"/> <!--
war 0.018 0.008 R1 (Bat - ADC input) = 22k, R2 (ADC input - GND)
=
2.2K--->
<define
name="VOLTAGE_OFFSET" value="0"
unit="V"/>
<define name="VoltageOfAdc(adc)"
value="(VOLTAGE_ADC_SCALE * adc + VOLTAGE_OFFSET)"/>
</section>
<!--#######################################################################################-->
<!--############################# MISCELLANEOUS
SETUP
###############################-->
<!--#######################################################################################-->
<section
name="MISC">
<define
name="CLIMB_AIRSPEED"
value="14."
unit="m/s"/>
<define
name="GLIDE_AIRSPEED"
value="14."
unit="m/s"/>
<define
name="RACE_AIRSPEED"
value="23."
unit="m/s"/>
<define
name="STALL_AIRSPEED"
value="12."
unit="m/s"/>
<define
name="AIRSPEED_SETPOINT_SLEW" value="1"
unit="s"/> <!--default=1-->
<define name="NOMINAL_AIRSPEED"
value="16"
unit="m/s"/>
<define name="MINIMUM_AIRSPEED" value="14."
unit="m/s"/>
<define name="MAXIMUM_AIRSPEED" value="26."
unit="m/s"/>
<define name="CARROT"
value="3."
unit="s"/>
<define
name="GLIDE_RATIO"
value="7."/>
<define
name="KILL_MODE_DISTANCE" value="(1.5*MAX_DIST_FROM_HOME)"/>
<define
name="CONTROL_FREQUENCY" 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="TRUE"/>
<define name="TRIGGER_DELAY"
value="1."/>
<define
name="DEFAULT_CIRCLE_RADIUS" value="120."/>
<define name="MIN_CIRCLE_RADIUS" value="100."/>
<define
name="UNLOCKED_HOME_MODE" value="TRUE"/>
<define name="RC_LOST_MODE"
value="PPRZ_MODE_AUTO2"/>
</section>
<section
name="AGGRESSIVE" prefix="AGR_">
<define name="BLEND_START"
value="40"/><!--
Altitude
Error to Initiate Aggressive Climb CANNOT BE ZERO!!-->
<define name="BLEND_END"
value="10"/><!--
Altitude
Error to Blend Aggressive to Regular Climb Modes NOT ZERO!!-->
<define name="CLIMB_THROTTLE"
value="1.0"/><!-- Gaz for
Aggressive Climb -->
<define
name="CLIMB_PITCH"
value="RadOfDeg(20)"/><!--
Pitch for Aggressive Climb -->
<define
name="DESCENT_THROTTLE"
value="0.1"/><!--
Gaz for Aggressive Decent -->
<define
name="DESCENT_PITCH"
value="RadOfDeg(-20)"/><!--
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="NAV">
<define name="NAV_PITCH" value="0."/>
<define
name="NAV_GLIDE_PITCH_TRIM" value="0"/>
<define
name="NAV_GROUND_SPEED_PGAIN" value="0.015"/>
<define
name="NAV_FOLLOW_PGAIN" value="-0.05"/>
</section>
<section name="GLS_APPROACH"
prefix="APP_">
<define
name="ANGLE" value="5"/>
<define name="INTERCEPT_AF_TOD"
value="10"/>
<define
name="TARGET_SPEED" value="13"/>
</section>
<section
name="FAILSAFE" prefix="FAILSAFE_">
<define
name="DELAY_WITHOUT_GPS" value="1"
unit="s"/>
<define
name="DEFAULT_THROTTLE"
value="0.6"
unit="%"/>
<define
name="DEFAULT_ROLL"
value="10"
unit="deg"/>
<define
name="DEFAULT_PITCH"
value="1"
unit="deg"/>
<define
name="HOME_RADIUS"
value="100"
unit="m"/>
<define
name="KILL_MODE_DISTANCE" value="(MAX_DIST_FROM_HOME*1.5)"/>
</section>
<section
name="DATALINK" prefix="DATALINK_">
<define name="DEVICE_TYPE"
value="PPRZ"/>
<define name="DEVICE_ADDRESS"
value="...."/>
</section>
<section name="DIGITAL_CAMERA"
prefix="DC_">
<define name="AUTOSHOOT_QUARTERSEC_PERIOD"
value="8" unit="quarter_second"/>
<define
name="AUTOSHOOT_METER_GRID" value="100"
unit="meter"/>
</section>
<section name="GCS">
<define name="ALT_SHIFT_PLUS_PLUS"
value="100"/>
<define name="ALT_SHIFT_PLUS"
value="10"/>
<define name="ALT_SHIFT_MINUS"
value="-10"/>
<define name="SPEECH_NAME"
value="Cessna"/>
</section>
<section name="SIMU">
<define name="WEIGHT" value
="1."/>
<define
name="YAW_RESPONSE_FACTOR" value =".9"/> <!--default
1.-->
<define name="PITCH_RESPONSE_FACTOR"
value ="1."/> <!--default 1.-->
<define
name="ROLL_RESPONSE_FACTOR" value ="15."/>
<!--default 15-->
</section>
<makefile>
</makefile>
</airframe>
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