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Fix compile warnings in ``make test`` (#3216)

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* Silent compile warnings in tests

* silent warnings in conf_test

* fix defines: if OLD -> warn and convert. If new, then use. If no old and no new, use default.
This commit is contained in:
Christophe De Wagter
2023-12-18 12:34:58 +01:00
committed by GitHub
parent f0d2cd3bdc
commit a07d674c19
6 changed files with 14 additions and 10 deletions
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conf/airframes/examples/bebop2_opticflow.xml
+3 -3
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@@ -277,9 +277,9 @@
<define name="FILT_CUTOFF_R" value="3.2"/>
<!-- first order actuator dynamics -->
<define name="ACT_DYN_P" value="0.06"/>
<define name="ACT_DYN_Q" value="0.06"/>
<define name="ACT_DYN_R" value="0.06"/>
<define name="ACT_FREQ_P" value="31.7"/>
<define name="ACT_FREQ_Q" value="31.7"/>
<define name="ACT_FREQ_R" value="31.7"/>
<!-- Adaptive Learning Rate -->
<define name="USE_ADAPTIVE" value="FALSE"/>
conf/airframes/examples/cube_orange.xml
+4 -3
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@@ -126,6 +126,7 @@
<define name="GUIDANCE_INDI_FILTER_CUTOFF" value="0.5"/>
<define name="GUIDANCE_INDI_LINE_GAIN" value="0.2"/>
<define name="GUIDANCE_INDI_MIN_THROTTLE" value="2500"/>
<define name="GUIDANCE_INDI_THRUST_DYNAMICS_FREQ" value="18"/>
</module>
<module name="motor_mixing"/>
@@ -300,9 +301,9 @@
<define name="FILT_CUTOFF_R" value="4.0"/>
<!-- first order actuator dynamics -->
<define name="ACT_DYN_P" value="0.0354"/>
<define name="ACT_DYN_Q" value="0.0354"/>
<define name="ACT_DYN_R" value="0.0354"/>
<define name="ACT_FREQ_P" value="18"/>
<define name="ACT_FREQ_Q" value="18"/>
<define name="ACT_FREQ_R" value="18"/>
<!-- Adaptive Learning Rate -->
<define name="USE_ADAPTIVE" value="FALSE"/>
conf/modules/imu_mpu9250_i2c.xml
+1
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@@ -42,6 +42,7 @@
<test>
<define name="IMU_MPU9250_I2C_DEV" value="i2c1"/>
<define name="USE_I2C1"/>
<define name="PERIODIC_FREQUENCY" value="512"/>
<define name="IMU_MPU9250_PERIODIC_FREQ" value="512"/>
</test>
</makefile>
conf/modules/imu_mpu9250_spi.xml
+1
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@@ -51,6 +51,7 @@
<define name="USE_SPI1"/>
<define name="IMU_MPU9250_SPI_SLAVE_IDX" value="0"/>
<define name="USE_SPI_SLAVE0"/>
<define name="PERIODIC_FREQUENCY" value="512"/>
<define name="IMU_MPU9250_PERIODIC_FREQ" value="512"/>
</test>
</makefile>
conf/modules/sensors_hitl.xml
+1 -1
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@@ -33,7 +33,7 @@
<file name="sensors_hitl.c"/>
<test firmware="rotorcraft">
<include name="../../conf/simulator/nps"/>
<define name="NPS_PROPAGATE" value="500"/>
<define name="AHRS_PROPAGATE_FREQUENCY" value="500"/>
<define name="HITL_DEVICE" value="usb_serial"/>
<define name="USE_USB_SERIAL"/>
</test>
sw/airborne/firmwares/rotorcraft/guidance/guidance_indi_hybrid.c
+4 -3
View File
@@ -128,13 +128,14 @@ static void guidance_indi_filter_thrust(void);
#warning "The thrust dynamics are now specified in continuous time with the corner frequency of the first order model!"
#warning "define GUIDANCE_INDI_THRUST_DYNAMICS_FREQ in rad/s"
#warning "Use -log(1 - old_number) * PERIODIC_FREQUENCY to compute it from the old value."
#define GUIDANCE_INDI_THRUST_DYNAMICS_FREQ (-ln(1-GUIDANCE_INDI_THRUST_DYNAMICS)*PERIODIC_FREQUENCY)
#endif
#ifndef GUIDANCE_INDI_THRUST_DYNAMICS_FREQ
#ifndef STABILIZATION_INDI_ACT_DYN_P
#error "You need to define GUIDANCE_INDI_THRUST_DYNAMICS to be able to use indi vertical control"
#ifndef STABILIZATION_INDI_ACT_FREQ_P
#error "You need to define GUIDANCE_INDI_THRUST_DYNAMICS_FREQ to be able to use indi vertical control"
#else // assume that the same actuators are used for thrust as for roll (e.g. quadrotor)
#define GUIDANCE_INDI_THRUST_DYNAMICS_FREQ STABILIZATION_INDI_ACT_DYN_P
#define GUIDANCE_INDI_THRUST_DYNAMICS_FREQ STABILIZATION_INDI_ACT_FREQ_P
#endif
#endif //GUIDANCE_INDI_THRUST_DYNAMICS_FREQ