-
Notifications
You must be signed in to change notification settings - Fork 1.1k
Commit
This commit does not belong to any branch on this repository, and may belong to a fork outside of the repository.
Support for TawakiV2 (STM32H7) (#3199)
* tawakiV2 support. * clean and update linker scripts * update ram configuration * update chibios * update airframe
- Loading branch information
Showing
28 changed files
with
4,331 additions
and
175 deletions.
There are no files selected for viewing
This file contains bidirectional Unicode text that may be interpreted or compiled differently than what appears below. To review, open the file in an editor that reveals hidden Unicode characters.
Learn more about bidirectional Unicode characters
This file contains bidirectional Unicode text that may be interpreted or compiled differently than what appears below. To review, open the file in an editor that reveals hidden Unicode characters.
Learn more about bidirectional Unicode characters
Original file line number | Diff line number | Diff line change |
---|---|---|
@@ -0,0 +1,228 @@ | ||
<!DOCTYPE airframe SYSTEM "../../airframe.dtd"> | ||
|
||
<airframe name="Cobra"> | ||
|
||
<description> | ||
* Autopilot: Tawaki | ||
* Actuators: 4 in 1 | ||
* Telemetry: XBee | ||
* GPS: datalink | ||
* RC: SBUS | ||
</description> | ||
|
||
<firmware name="rotorcraft"> | ||
<!--configure name="RTOS_DEBUG" value="TRUE"/--> | ||
<configure name="PERIODIC_FREQUENCY" value="500"/> | ||
<configure name="AHRS_PROPAGATE_FREQUENCY" value="$(PERIODIC_FREQUENCY)"/> | ||
|
||
<target name="ap" board="tawaki_1.1"> | ||
<module name="radio_control" type="sbus"/> | ||
<configure name="BARO_PERIODIC_FREQUENCY" value="50"/> | ||
<define name="RADIO_KILL_SWITCH" value="RADIO_GAIN1"/> | ||
</target> | ||
<target name="nps" board="pc"> | ||
<module name="fdm" type="jsbsim"/> | ||
<module name="radio_control" type="ppm"/> | ||
</target> | ||
|
||
<module name="telemetry" type="xbee_api"/> | ||
<!--module name="telemetry" type="transparent"> | ||
<configure name="MODEM_PORT" value="usb_serial"/> | ||
</module--> | ||
|
||
<module name="actuators" type="dshot"/> | ||
<module name="actuators" type="pwm"/> | ||
<module name="switch" type="servo"/> | ||
<define name="SWITCH_SERVO_ON_VALUE" value="SERVO_SWITCH_MAX"/> | ||
<define name="SWITCH_SERVO_OFF_VALUE" value="SERVO_SWITCH_MIN"/> | ||
|
||
<module name="board" type="tawaki"> | ||
<define name="IMU_MPU_LOWPASS_FILTER" value="MPU60X0_DLPF_256HZ"/> | ||
<define name="IMU_MPU_ACCEL_LOWPASS_FILTER" value="MPU60X0_DLPF_ACC_218HZ"/> | ||
<define name="IMU_MPU_SMPLRT_DIV" value="0"/> | ||
</module> | ||
|
||
<!--module name="gps" type="ublox"> | ||
<configure name="GPS_BAUD" value="B115200"/> | ||
<define name="USE_GPS_UBX_RTCM" value="TRUE"/> | ||
<define name="GPS_FIX_TIMEOUT" value="0.5"/> | ||
</module--> | ||
<module name="gps" type="optitrack"/> | ||
|
||
<module name="stabilization" type="indi"/> | ||
<module name="guidance" type="indi"/> | ||
|
||
<module name="ins" type="ekf2"> | ||
<define name="INS_EKF2_OPTITRACK" value="TRUE"/> | ||
</module> | ||
<module name="preflight_checks"/> | ||
|
||
<!--module name="filter" type="1euro_imu"> | ||
<define name="AHRS_ICQ_IMU_ID" value="IMU_F1E_ID"/> | ||
<define name="AHRS_ALIGNER_IMU_ID" value="IMU_F1E_ID"/> | ||
</module--> | ||
|
||
<module name="motor_mixing"/> | ||
|
||
<module name="tag_tracking"> | ||
<configure name="JEVOIS_UART" value="UART3"/> | ||
</module> | ||
|
||
<module name="flight_recorder"/> | ||
</firmware> | ||
|
||
<servos driver="Pwm"> | ||
<servo name="SWITCH" no="1" min="800" neutral="800" max="1500"/> | ||
</servos> | ||
|
||
<servos driver="DShot"> | ||
<servo name="FR" no="3" min="0" neutral="100" max="2000"/> | ||
<servo name="BR" no="4" min="0" neutral="100" max="2000"/> | ||
<servo name="BL" no="2" min="0" neutral="100" max="2000"/> | ||
<servo name="FL" no="1" min="0" neutral="100" max="2000"/> | ||
</servos> | ||
|
||
<commands> | ||
<axis name="ROLL" failsafe_value="0"/> | ||
<axis name="PITCH" failsafe_value="0"/> | ||
<axis name="YAW" failsafe_value="0"/> | ||
<axis name="THRUST" failsafe_value="0"/> | ||
</commands> | ||
|
||
<section name="MIXING" prefix="MOTOR_MIXING_"> | ||
<define name="TYPE" value="QUAD_X"/> | ||
<define name="REVERSE" value="TRUE"/> | ||
</section> | ||
|
||
<command_laws> | ||
<set servo="FR" value="autopilot_get_motors_on() ? actuators_pprz[0] : -MAX_PPRZ"/> | ||
<set servo="BR" value="autopilot_get_motors_on() ? actuators_pprz[1] : -MAX_PPRZ"/> | ||
<set servo="BL" value="autopilot_get_motors_on() ? actuators_pprz[2] : -MAX_PPRZ"/> | ||
<set servo="FL" value="autopilot_get_motors_on() ? actuators_pprz[3] : -MAX_PPRZ"/> | ||
</command_laws> | ||
|
||
<section name="IMU" prefix="IMU_"> | ||
<define name="ACCEL_CALIB" value="{{.abi_id=9, .calibrated={.neutral=true, .scale=true},.neutral={-12,23,29}, .scale={{65369,62166,40813},{28737,25351,16753}}}}"/> | ||
<!--define name="MAG_CALIB" value="{{.abi_id=3, .calibrated={.neutral=true, .scale=true},.neutral={-833,-5969,-931}, .scale={{22816,38799,15650},{34941,60353,24187}}}}"/--> | ||
|
||
<define name="BODY_TO_IMU_PHI" value="0." unit="deg"/> | ||
<define name="BODY_TO_IMU_THETA" value="0." unit="deg"/> | ||
<define name="BODY_TO_IMU_PSI" value="180." unit="deg"/> | ||
</section> | ||
|
||
<include href="conf/mag/toulouse_muret.xml"/> | ||
|
||
<section name="STABILIZATION_ATTITUDE" 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="60" unit="deg/s"/> | ||
<define name="DEADBAND_A" value="0"/> | ||
<define name="DEADBAND_E" value="0"/> | ||
<define name="DEADBAND_R" value="50"/> | ||
</section> | ||
|
||
<section name="STABILIZATION_ATTITUDE_INDI" prefix="STABILIZATION_INDI_"> | ||
<define name="NUM_ACT" value="4"/> | ||
<!-- reference acceleration for attitude control --> | ||
<define name="REF_ERR_P" value="120"/> | ||
<define name="REF_ERR_Q" value="130"/> | ||
<define name="REF_ERR_R" value="120"/> | ||
<define name="REF_RATE_P" value="15"/> | ||
<define name="REF_RATE_Q" value="15"/> | ||
<define name="REF_RATE_R" value="10"/> | ||
<define name="MAX_R" value="60" unit="deg/s"/> | ||
|
||
<!-- second order filter parameters --> | ||
<define name="FILT_CUTOFF" value="4.0"/> | ||
<define name="FILT_CUTOFF_R" value="4.0"/> | ||
|
||
<!-- Adaptive Learning Rate --> | ||
<define name="USE_ADAPTIVE" value="FALSE"/> | ||
<define name="ADAPTIVE_MU" value="0.0001"/> | ||
|
||
<!-- Full INDI --> | ||
<!-- control effectiveness --> | ||
<define name="G1_ROLL" value="{ -20.0, -20.0, 20.0, 20.0 }"/> | ||
<define name="G1_PITCH" value="{ 20.0, -20.0, -20.0, 20.0 }"/> | ||
<define name="G1_YAW" value="{ 3, -3, 3, -3 }"/> | ||
<define name="G1_THRUST" value="{ -1., -1., -1., -1.}"/> | ||
<!--Counter torque effect of spinning up a rotor--> | ||
<define name="G2" value="{80, -80, 80, -80.0 }"/> | ||
<!-- first order actuator dynamics --> | ||
<define name="ACT_FREQ" value="{10.10, 10.10, 10.10, 10.10}"/> | ||
<define name="ESTIMATION_FILT_CUTOFF" value="4.0"/> | ||
<!--Priority for each axis (roll, pitch, yaw and thrust)--> | ||
<define name="WLS_PRIORITIES" value="{1000, 1000, 1, 100}"/> | ||
</section> | ||
|
||
<section name="GUIDANCE_V" prefix="GUIDANCE_V_"> | ||
<define name="REF_MIN_ZDD" value="-0.4*9.81"/> | ||
<define name="REF_MAX_ZDD" value=" 0.4*9.81"/> | ||
<define name="REF_MIN_ZD" value="-2."/> | ||
<define name="REF_MAX_ZD" value=" 2."/> | ||
<define name="HOVER_KP" value="90"/> | ||
<define name="HOVER_KD" value="110"/> | ||
<define name="HOVER_KI" value="10"/> | ||
<define name="NOMINAL_HOVER_THROTTLE" value="0.35"/> | ||
<define name="ADAPT_THROTTLE_ENABLED" value="TRUE"/> | ||
<define name="ADAPT_NOISE_FACTOR" value="1."/> | ||
<define name="ADAPT_INITIAL_HOVER_THROTTLE" value="0.3"/> | ||
</section> | ||
|
||
<section name="GUIDANCE_H" prefix="GUIDANCE_H_"> | ||
<define name="MAX_BANK" value="30" unit="deg"/> | ||
<define name="PGAIN" value="41"/> | ||
<define name="DGAIN" value="108"/> | ||
<define name="IGAIN" value="20"/> | ||
<define name="NGAIN" value="0"/> | ||
<!-- feedforward --> | ||
<define name="AGAIN" value="0"/> | ||
<define name="REF_MAX_SPEED" value="0.5"/> | ||
<define name="REF_MAX_ACCEL" value="2."/> | ||
</section> | ||
|
||
<section name="GUIDANCE_INDI" prefix="GUIDANCE_INDI_"> | ||
<define name="SPECIFIC_FORCE_GAIN" value="-500.0"/> | ||
<define name="THRUST_DYNAMICS_FREQ" value="25.64"/> | ||
<define name="RC_DEBUG" value="FALSE"/> | ||
<define name="SPEED_GAINZ" value="2.5"/> | ||
</section> | ||
|
||
<section name="NAV"> | ||
<define name="ARRIVED_AT_WAYPOINT" value="0.25"/> | ||
<define name="NAV_CLIMB_VSPEED" value="0.8"/> | ||
<define name="NAV_DESCEND_VSPEED" value="-0.5"/> | ||
<define name="NAV_CARROT_DIST" value="18"/> | ||
</section> | ||
|
||
<section name="BAT"> | ||
<define name="CRITIC_BAT_LEVEL" value="9.3" unit="V"/> | ||
</section> | ||
|
||
<section name="AUTOPILOT"> | ||
<define name="MODE_STARTUP" value="AP_MODE_NAV"/> | ||
<define name="MODE_MANUAL" value="AP_MODE_ATTITUDE_DIRECT"/> | ||
<define name="MODE_AUTO1" value="AP_MODE_ATTITUDE_Z_HOLD"/> | ||
<define name="MODE_AUTO2" value="AP_MODE_NAV"/> | ||
<define name="FAILSAFE_FIXED_THROTTLE" value="0.4"/> | ||
</section> | ||
|
||
<section name="TAG_TRACKING" prefix="TAG_TRACKING_"> | ||
<define name="BODY_TO_CAM_PSI" value="M_PI_2"/> | ||
<define name="CAM_POS_X" value="0.15"/> | ||
</section> | ||
|
||
<section name="GCS"> | ||
<define name="ALT_SHIFT_PLUS_PLUS" value="3"/> | ||
<define name="ALT_SHIFT_PLUS" value="1"/> | ||
<define name="ALT_SHIFT_MINUS" value="-0.5"/> | ||
</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"/> | ||
</section> | ||
|
||
</airframe> | ||
|
Oops, something went wrong.