Merge branch 'master' of github.com:PX4/Firmware into pca8574

This commit is contained in:
Lorenz Meier
2014-05-29 11:26:18 +02:00
292 changed files with 9635 additions and 12192 deletions
+2
View File
@@ -37,3 +37,5 @@ mavlink/include/mavlink/v0.9/
tags
.tags_sorted_by_file
.pydevproject
.ropeproject
*.orig
Binary file not shown.
Binary file not shown.
+12
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@@ -0,0 +1,12 @@
{
"board_id": 19,
"magic": "AeroCore",
"description": "Firmware for the Gumstix AeroCore board",
"image": "",
"build_time": 0,
"summary": "AEROCORE",
"version": "0.1",
"image_size": 0,
"git_identity": "",
"board_revision": 0
}
+3 -3
View File
@@ -18,9 +18,9 @@ then
param set MC_PITCHRATE_P 0.13
param set MC_PITCHRATE_I 0.0
param set MC_PITCHRATE_D 0.004
param set MC_YAW_P 0.5
param set MC_YAWRATE_P 0.2
param set MC_YAWRATE_I 0.0
param set MC_YAW_P 2.5
param set MC_YAWRATE_P 0.25
param set MC_YAWRATE_I 0.25
param set MC_YAWRATE_D 0.0
param set BAT_V_SCALING 0.00989
@@ -0,0 +1,35 @@
#!nsh
#
# Steadidrone QU4D
#
# Thomas Gubler <thomasgubler@gmail.com>
# Lorenz Meier <lm@inf.ethz.ch>
#
sh /etc/init.d/rc.mc_defaults
if [ $DO_AUTOCONFIG == yes ]
then
# TODO tune roll/pitch separately
param set MC_ROLL_P 7.0
param set MC_ROLLRATE_P 0.13
param set MC_ROLLRATE_I 0.0
param set MC_ROLLRATE_D 0.004
param set MC_PITCH_P 7.0
param set MC_PITCHRATE_P 0.13
param set MC_PITCHRATE_I 0.0
param set MC_PITCHRATE_D 0.004
param set MC_YAW_P 0.5
param set MC_YAWRATE_P 0.2
param set MC_YAWRATE_I 0.0
param set MC_YAWRATE_D 0.0
param set BAT_N_CELLS 4
fi
set MIXER FMU_quad_w
set PWM_MIN 1210
set PWM_MAX 2100
set PWM_OUTPUTS 1234
@@ -1,7 +1,5 @@
#!nsh
#
# UNTESTED UNTESTED!
#
# Generic 10" Hexa coaxial geometry
#
# Lorenz Meier <lm@inf.ethz.ch>
+1 -1
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@@ -5,4 +5,4 @@
sh /etc/init.d/rc.fw_defaults
set MIXER FMU_RET
set MIXER easystar
+13 -12
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@@ -14,19 +14,20 @@ sh /etc/init.d/rc.mc_defaults
if [ $DO_AUTOCONFIG == yes ]
then
# Set all params here, then disable autoconfig
param set MC_ROLL_P 5.0
param set MC_ROLLRATE_P 0.13
param set MC_ROLLRATE_I 0.0
param set MC_ROLLRATE_D 0.0
param set MC_PITCH_P 5.0
param set MC_PITCHRATE_P 0.13
param set MC_PITCHRATE_I 0.0
param set MC_PITCHRATE_D 0.0
param set MC_YAW_P 1.0
param set MC_YAWRATE_P 0.15
param set MC_YAWRATE_I 0.0
param set MC_ROLL_P 6.0
param set MC_ROLLRATE_P 0.14
param set MC_ROLLRATE_I 0.1
param set MC_ROLLRATE_D 0.002
param set MC_PITCH_P 6.0
param set MC_PITCHRATE_P 0.14
param set MC_PITCHRATE_I 0.1
param set MC_PITCHRATE_D 0.002
param set MC_YAW_P 2.0
param set MC_YAWRATE_P 0.2
param set MC_YAWRATE_I 0.2
param set MC_YAWRATE_D 0.0
param set MC_YAW_FF 0.15
param set MC_YAW_FF 0.8
param set BAT_V_SCALING 0.00838095238
fi
+5
View File
@@ -195,6 +195,11 @@ then
sh /etc/init.d/10016_3dr_iris
fi
if param compare SYS_AUTOSTART 10017
then
sh /etc/init.d/10017_steadidrone_qu4d
fi
#
# Hexa Coaxial
#
+1 -1
View File
@@ -6,7 +6,7 @@
#
# Start the attitude and position estimator
#
fw_att_pos_estimator start
ekf_att_pos_estimator start
#
# Start attitude controller
@@ -11,6 +11,4 @@ then
param set NAV_RTL_ALT 100
param set NAV_RTL_LAND_T -1
param set NAV_ACCEPT_RAD 50
param set RC_SCALE_ROLL 1
param set RC_SCALE_PITCH 1
fi
+1 -1
View File
@@ -11,7 +11,7 @@ px4io recovery
# Adjust PX4IO update rate limit
#
set PX4IO_LIMIT 400
if hw_ver compare PX4FMU_V1
if ver hwcmp PX4FMU_V1
then
set PX4IO_LIMIT 200
fi
+3 -3
View File
@@ -5,12 +5,12 @@
if [ -d /fs/microsd ]
then
if hw_ver compare PX4FMU_V1
if ver hwcmp PX4FMU_V1
then
echo "Start sdlog2 at 50Hz"
sdlog2 start -r 50 -a -b 8 -t
sdlog2 start -r 50 -a -b 4 -t
else
echo "Start sdlog2 at 200Hz"
sdlog2 start -r 200 -a -b 16 -t
sdlog2 start -r 200 -a -b 22 -t
fi
fi
+1
View File
@@ -5,6 +5,7 @@
#
attitude_estimator_ekf start
#ekf_att_pos_estimator start
position_estimator_inav start
mc_att_control start
+8 -2
View File
@@ -32,9 +32,15 @@ then
param set MPC_Z_VEL_D 0.0
param set MPC_Z_VEL_MAX 3
param set MPC_Z_FF 0.5
param set MPC_TILT_MAX 1.0
param set MPC_TILTMAX_AIR 45.0
param set MPC_TILTMAX_LND 15.0
param set MPC_LAND_SPEED 1.0
param set MPC_LAND_TILT 0.3
param set PE_VELNE_NOISE 0.5
param set PE_VELNE_NOISE 0.7
param set PE_POSNE_NOISE 0.5
param set PE_POSD_NOISE 1.0
fi
set PWM_RATE 400
+1 -1
View File
@@ -22,7 +22,7 @@ then
echo "[init] Using L3GD20(H)"
fi
if hw_ver compare PX4FMU_V2
if ver hwcmp PX4FMU_V2
then
if lsm303d start
then
+7 -3
View File
@@ -3,16 +3,20 @@
# USB MAVLink start
#
echo "Starting MAVLink on this USB console"
mavlink start -r 10000 -d /dev/ttyACM0
# Enable a number of interesting streams we want via USB
mavlink stream -d /dev/ttyACM0 -s NAMED_VALUE_FLOAT -r 10
usleep 100000
mavlink stream -d /dev/ttyACM0 -s OPTICAL_FLOW -r 10
usleep 100000
mavlink stream -d /dev/ttyACM0 -s VFR_HUD -r 20
usleep 100000
mavlink stream -d /dev/ttyACM0 -s ATTITUDE -r 20
usleep 100000
mavlink stream -d /dev/ttyACM0 -s ATTITUDE_CONTROLS -r 30
mavlink stream -d /dev/ttyACM0 -s SERVO_OUTPUT_RAW_0 -r 10
usleep 100000
mavlink stream -d /dev/ttyACM0 -s SERVO_OUTPUT_RAW_0 -r 20
usleep 100000
# Exit shell to make it available to MAVLink
exit
+14 -14
View File
@@ -248,7 +248,7 @@ then
echo "[init] ERROR: PX4IO not found, disabling output"
# Avoid using ttyS0 for MAVLink on FMUv1
if hw_ver compare PX4FMU_V1
if ver hwcmp PX4FMU_V1
then
set FMU_MODE serial
fi
@@ -262,7 +262,7 @@ then
if [ $HIL == yes ]
then
set OUTPUT_MODE hil
if hw_ver compare PX4FMU_V1
if ver hwcmp PX4FMU_V1
then
set FMU_MODE serial
fi
@@ -308,7 +308,7 @@ then
tone_alarm $TUNE_OUT_ERROR
fi
if hw_ver compare PX4FMU_V1
if ver hwcmp PX4FMU_V1
then
if [ $FMU_MODE == pwm -o $FMU_MODE == gpio ]
then
@@ -383,7 +383,7 @@ then
tone_alarm $TUNE_OUT_ERROR
fi
if hw_ver compare PX4FMU_V1
if ver hwcmp PX4FMU_V1
then
if [ $FMU_MODE == pwm -o $FMU_MODE == gpio ]
then
@@ -419,16 +419,6 @@ then
mavlink start $MAVLINK_FLAGS
#
# Start the datamanager
#
dataman start
#
# Start the navigator
#
navigator start
#
# Sensors, Logging, GPS
#
@@ -550,6 +540,16 @@ then
fi
fi
#
# Start the datamanager
#
dataman start
#
# Start the navigator
#
navigator start
#
# Generic setup (autostart ID not found)
#
+154
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@@ -0,0 +1,154 @@
PX4 mixer definitions
=====================
Files in this directory implement example mixers that can be used as a basis
for customisation, or for general testing purposes.
Mixer basics
------------
Mixers combine control values from various sources (control tasks, user inputs,
etc.) and produce output values suitable for controlling actuators; servos,
motors, switches and so on.
An actuator derives its value from the combination of one or more control
values. Each of the control values is scaled according to the actuator's
configuration and then combined to produce the actuator value, which may then be
further scaled to suit the specific output type.
Internally, all scaling is performed using floating point values. Inputs and
outputs are clamped to the range -1.0 to 1.0.
control control control
| | |
v v v
scale scale scale
| | |
| v |
+-------> mix <------+
|
scale
|
v
out
Scaling
-------
Basic scalers provide linear scaling of the input to the output.
Each scaler allows the input value to be scaled independently for inputs
greater/less than zero. An offset can be applied to the output, and lower and
upper boundary constraints can be applied. Negative scaling factors cause the
output to be inverted (negative input produces positive output).
Scaler pseudocode:
if (input < 0)
output = (input * NEGATIVE_SCALE) + OFFSET
else
output = (input * POSITIVE_SCALE) + OFFSET
if (output < LOWER_LIMIT)
output = LOWER_LIMIT
if (output > UPPER_LIMIT)
output = UPPER_LIMIT
Syntax
------
Mixer definitions are text files; lines beginning with a single capital letter
followed by a colon are significant. All other lines are ignored, meaning that
explanatory text can be freely mixed with the definitions.
Each file may define more than one mixer; the allocation of mixers to actuators
is specific to the device reading the mixer definition, and the number of
actuator outputs generated by a mixer is specific to the mixer.
A mixer begins with a line of the form
<tag>: <mixer arguments>
The tag selects the mixer type; 'M' for a simple summing mixer, 'R' for a
multirotor mixer, etc.
Null Mixer
..........
A null mixer consumes no controls and generates a single actuator output whose
value is always zero. Typically a null mixer is used as a placeholder in a
collection of mixers in order to achieve a specific pattern of actuator outputs.
The null mixer definition has the form:
Z:
Simple Mixer
............
A simple mixer combines zero or more control inputs into a single actuator
output. Inputs are scaled, and the mixing function sums the result before
applying an output scaler.
A simple mixer definition begins with:
M: <control count>
O: <-ve scale> <+ve scale> <offset> <lower limit> <upper limit>
If <control count> is zero, the sum is effectively zero and the mixer will
output a fixed value that is <offset> constrained by <lower limit> and <upper
limit>.
The second line defines the output scaler with scaler parameters as discussed
above. Whilst the calculations are performed as floating-point operations, the
values stored in the definition file are scaled by a factor of 10000; i.e. an
offset of -0.5 is encoded as -5000.
The definition continues with <control count> entries describing the control
inputs and their scaling, in the form:
S: <group> <index> <-ve scale> <+ve scale> <offset> <lower limit> <upper limit>
The <group> value identifies the control group from which the scaler will read,
and the <index> value an offset within that group. These values are specific to
the device reading the mixer definition.
When used to mix vehicle controls, mixer group zero is the vehicle attitude
control group, and index values zero through three are normally roll, pitch,
yaw and thrust respectively.
The remaining fields on the line configure the control scaler with parameters as
discussed above. Whilst the calculations are performed as floating-point
operations, the values stored in the definition file are scaled by a factor of
10000; i.e. an offset of -0.5 is encoded as -5000.
Multirotor Mixer
................
The multirotor mixer combines four control inputs (roll, pitch, yaw, thrust)
into a set of actuator outputs intended to drive motor speed controllers.
The mixer definition is a single line of the form:
R: <geometry> <roll scale> <pitch scale> <yaw scale> <deadband>
The supported geometries include:
4x - quadrotor in X configuration
4+ - quadrotor in + configuration
6x - hexcopter in X configuration
6+ - hexcopter in + configuration
8x - octocopter in X configuration
8+ - octocopter in + configuration
Each of the roll, pitch and yaw scale values determine scaling of the roll,
pitch and yaw controls relative to the thrust control. Whilst the calculations
are performed as floating-point operations, the values stored in the definition
file are scaled by a factor of 10000; i.e. an factor of 0.5 is encoded as 5000.
Roll, pitch and yaw inputs are expected to range from -1.0 to 1.0, whilst the
thrust input ranges from 0.0 to 1.0. Output for each actuator is in the
range -1.0 to 1.0.
In the case where an actuator saturates, all actuator values are rescaled so that
the saturating actuator is limited to 1.0.
+31
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@@ -0,0 +1,31 @@
EASYSTAR / EASYSTAR II MIXER
============================
Aileron mixer
-------------
One output - would be easy to add support for 2 servos
M: 1
O: 10000 10000 0 -10000 10000
S: 0 0 10000 10000 0 -10000 10000
Elevator mixer
------------
M: 1
O: 10000 10000 0 -10000 10000
S: 0 1 -10000 -10000 0 -10000 10000
Rudder mixer
------------
M: 1
O: 10000 10000 0 -10000 10000
S: 0 2 -10000 -10000 0 -10000 10000
Motor speed mixer
-----------------
M: 1
O: 10000 10000 0 -10000 10000
S: 0 3 0 20000 -10000 -10000 10000
+2 -1
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@@ -16,5 +16,6 @@ astyle \
--ignore-exclude-errors-x \
--lineend=linux \
--exclude=EASTL \
--add-brackets \
--add-brackets \
--max-code-length=120 \
$*
+15 -14
View File
@@ -43,29 +43,30 @@ from __future__ import print_function
import argparse
import os
def main():
# Parse commandline arguments
parser = argparse.ArgumentParser(description="ROMFS pruner.")
parser.add_argument('--folder', action="store", help="ROMFS scratch folder.")
args = parser.parse_args()
print("Pruning ROMFS files.")
# go through
# go through
for (root, dirs, files) in os.walk(args.folder):
for file in files:
# only prune text files
if ".zip" in file or ".bin" in file:
if ".zip" in file or ".bin" in file or ".swp" in file:
continue
file_path = os.path.join(root, file)
file_path = os.path.join(root, file)
# read file line by line
pruned_content = ""
with open(file_path, "r") as f:
for line in f:
for line in f:
# handle mixer files differently than startup files
if file_path.endswith(".mix"):
if line.startswith(("Z:", "M:", "R: ", "O:", "S:")):
@@ -73,11 +74,11 @@ def main():
else:
if not line.isspace() and not line.strip().startswith("#"):
pruned_content += line
# overwrite old scratch file
with open(file_path, "w") as f:
f.write(pruned_content)
if __name__ == '__main__':
main()
main()
+2
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@@ -1,2 +1,4 @@
./obj/*
mixer_test
sbus2_test
autodeclination_test
+26 -34
View File
@@ -1,47 +1,39 @@
CC=g++
CFLAGS=-I. -I../../src/modules -I ../../src/include -I../../src/drivers -I../../src -D__EXPORT="" -Dnullptr="0"
CFLAGS=-I. -I../../src/modules -I ../../src/include -I../../src/drivers \
-I../../src -I../../src/lib -D__EXPORT="" -Dnullptr="0" -lm
ODIR=obj
LDIR =../lib
all: mixer_test sbus2_test autodeclination_test
LIBS=-lm
MIXER_FILES=../../src/systemcmds/tests/test_mixer.cpp \
../../src/systemcmds/tests/test_conv.cpp \
../../src/modules/systemlib/mixer/mixer_simple.cpp \
../../src/modules/systemlib/mixer/mixer_multirotor.cpp \
../../src/modules/systemlib/mixer/mixer.cpp \
../../src/modules/systemlib/mixer/mixer_group.cpp \
../../src/modules/systemlib/mixer/mixer_load.c \
../../src/modules/systemlib/pwm_limit/pwm_limit.c \
hrt.cpp \
mixer_test.cpp
#_DEPS = test.h
#DEPS = $(patsubst %,$(IDIR)/%,$(_DEPS))
SBUS2_FILES=../../src/modules/px4iofirmware/sbus.c \
hrt.cpp \
sbus2_test.cpp
_OBJ = mixer_test.o test_mixer.o mixer_simple.o mixer_multirotor.o \
mixer.o mixer_group.o mixer_load.o test_conv.o pwm_limit.o hrt.o
OBJ = $(patsubst %,$(ODIR)/%,$(_OBJ))
AUTODECLINATION_FILES= ../../src/lib/geo/geo_mag_declination.c \
hrt.cpp \
autodeclination_test.cpp
#$(DEPS)
$(ODIR)/%.o: %.cpp
mkdir -p obj
$(CC) -c -o $@ $< $(CFLAGS)
mixer_test: $(MIXER_FILES)
$(CC) -o mixer_test $(MIXER_FILES) $(CFLAGS)
$(ODIR)/%.o: ../../src/systemcmds/tests/%.cpp
$(CC) -c -o $@ $< $(CFLAGS)
sbus2_test: $(SBUS2_FILES)
$(CC) -o sbus2_test $(SBUS2_FILES) $(CFLAGS)
$(ODIR)/%.o: ../../src/modules/systemlib/%.cpp
$(CC) -c -o $@ $< $(CFLAGS)
$(ODIR)/%.o: ../../src/modules/systemlib/mixer/%.cpp
$(CC) -c -o $@ $< $(CFLAGS)
$(ODIR)/%.o: ../../src/modules/systemlib/pwm_limit/%.cpp
$(CC) -c -o $@ $< $(CFLAGS)
$(ODIR)/%.o: ../../src/modules/systemlib/pwm_limit/%.c
$(CC) -c -o $@ $< $(CFLAGS)
$(ODIR)/%.o: ../../src/modules/systemlib/mixer/%.c
$(CC) -c -o $@ $< $(CFLAGS)
#
mixer_test: $(OBJ)
g++ -o $@ $^ $(CFLAGS) $(LIBS)
autodeclination_test: $(SBUS2_FILES)
$(CC) -o autodeclination_test $(AUTODECLINATION_FILES) $(CFLAGS)
.PHONY: clean
clean:
rm -f $(ODIR)/*.o *~ core $(INCDIR)/*~
rm -f $(ODIR)/*.o *~ core $(INCDIR)/*~ mixer_test sbus2_test autodeclination_test
+28
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@@ -0,0 +1,28 @@
#include <stdio.h>
#include <stdlib.h>
#include <unistd.h>
#include <string.h>
#include <systemlib/mixer/mixer.h>
#include <systemlib/err.h>
#include <drivers/drv_hrt.h>
#include <px4iofirmware/px4io.h>
#include "../../src/systemcmds/tests/tests.h"
#include <geo/geo.h>
int main(int argc, char *argv[]) {
warnx("autodeclination test started");
if (argc < 3)
errx(1, "Need lat/lon!");
char* p_end;
float lat = strtod(argv[1], &p_end);
float lon = strtod(argv[2], &p_end);
float declination = get_mag_declination(lat, lon);
printf("lat: %f lon: %f, dec: %f\n", lat, lon, declination);
}
View File
+5
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@@ -0,0 +1,5 @@
#pragma once
#include <systemlib/err.h>
#define lowsyslog warnx
+1 -1
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@@ -11,4 +11,4 @@ int main(int argc, char *argv[]) {
test_mixer(3, args);
test_conv(1, args);
}
}
+6
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@@ -0,0 +1,6 @@
#!/bin/sh
make clean
make all
./mixer_test
./sbus2_test ../../../../data/sbus2/sbus2_r7008SB_gps_baro_tx_off.txt
+75
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@@ -0,0 +1,75 @@
#include <stdio.h>
#include <unistd.h>
#include <string.h>
#include <systemlib/mixer/mixer.h>
#include <systemlib/err.h>
#include <drivers/drv_hrt.h>
#include <px4iofirmware/px4io.h>
#include "../../src/systemcmds/tests/tests.h"
int main(int argc, char *argv[]) {
warnx("SBUS2 test started");
if (argc < 2)
errx(1, "Need a filename for the input file");
warnx("loading data from: %s", argv[1]);
FILE *fp;
fp = fopen(argv[1],"rt");
if (!fp)
errx(1, "failed opening file");
float f;
unsigned x;
int ret;
// Trash the first 20 lines
for (unsigned i = 0; i < 20; i++) {
(void)fscanf(fp, "%f,%x,,", &f, &x);
}
// Init the parser
uint8_t frame[30];
unsigned partial_frame_count = 0;
uint16_t rc_values[18];
uint16_t num_values;
bool sbus_failsafe;
bool sbus_frame_drop;
uint16_t max_channels = sizeof(rc_values) / sizeof(rc_values[0]);
float last_time = 0;
while (EOF != (ret = fscanf(fp, "%f,%x,,", &f, &x))) {
if (((f - last_time) * 1000 * 1000) > 3000) {
partial_frame_count = 0;
warnx("FRAME RESET\n\n");
}
frame[partial_frame_count] = x;
partial_frame_count++;
//warnx("%f: 0x%02x, first: 0x%02x, last: 0x%02x, pcount: %u", (double)f, x, frame[0], frame[24], partial_frame_count);
if (partial_frame_count == sizeof(frame))
partial_frame_count = 0;
last_time = f;
// Pipe the data into the parser
hrt_abstime now = hrt_absolute_time();
//if (partial_frame_count % 25 == 0)
//sbus_parse(now, frame, &partial_frame_count, rc_values, &num_values, &sbus_failsafe, &sbus_frame_drop, max_channels);
}
if (ret == EOF) {
warnx("Test finished, reached end of file");
} else {
warnx("Test aborted, errno: %d", ret);
}
}
+11
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@@ -0,0 +1,11 @@
#
# Board-specific definitions for the Gumstix AeroCore
#
#
# Configure the toolchain
#
CONFIG_ARCH = CORTEXM4F
CONFIG_BOARD = AEROCORE
include $(PX4_MK_DIR)/toolchain_gnu-arm-eabi.mk
+125
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@@ -0,0 +1,125 @@
#
# Makefile for the AeroCore *default* configuration
#
#
# Use the configuration's ROMFS.
#
ROMFS_ROOT = $(PX4_BASE)/ROMFS/px4fmu_common
#
# Board support modules
#
MODULES += drivers/device
MODULES += drivers/stm32
MODULES += drivers/stm32/adc
MODULES += drivers/stm32/tone_alarm
MODULES += drivers/led
MODULES += drivers/px4fmu
MODULES += drivers/boards/aerocore
MODULES += drivers/lsm303d
MODULES += drivers/l3gd20
MODULES += drivers/ms5611
MODULES += drivers/gps
MODULES += drivers/hil
MODULES += modules/sensors
#
# System commands
#
MODULES += systemcmds/boardinfo
MODULES += systemcmds/mixer
MODULES += systemcmds/param
MODULES += systemcmds/perf
MODULES += systemcmds/preflight_check
MODULES += systemcmds/pwm
MODULES += systemcmds/esc_calib
MODULES += systemcmds/reboot
MODULES += systemcmds/top
MODULES += systemcmds/config
MODULES += systemcmds/nshterm
MODULES += systemcmds/mtd
MODULES += systemcmds/dumpfile
#
# General system control
#
MODULES += modules/commander
MODULES += modules/navigator
MODULES += modules/mavlink
#
# Estimation modules (EKF/ SO3 / other filters)
#
MODULES += modules/attitude_estimator_ekf
MODULES += modules/attitude_estimator_so3
MODULES += modules/ekf_att_pos_estimator
MODULES += modules/position_estimator_inav
#
# Vehicle Control
#
MODULES += modules/fw_pos_control_l1
MODULES += modules/fw_att_control
MODULES += modules/mc_att_control
MODULES += modules/mc_pos_control
#
# Library modules
#
MODULES += modules/systemlib
MODULES += modules/systemlib/mixer
MODULES += modules/controllib
MODULES += modules/uORB
MODULES += modules/dataman
#
# Libraries
#
LIBRARIES += lib/mathlib/CMSIS
MODULES += lib/mathlib
MODULES += lib/mathlib/math/filter
MODULES += lib/ecl
MODULES += lib/external_lgpl
MODULES += lib/geo
MODULES += lib/conversion
MODULES += lib/launchdetection
#
# Demo apps
#
#MODULES += examples/math_demo
# Tutorial code from
# https://pixhawk.ethz.ch/px4/dev/hello_sky
MODULES += examples/px4_simple_app
# Tutorial code from
# https://pixhawk.ethz.ch/px4/dev/daemon
#MODULES += examples/px4_daemon_app
# Tutorial code from
# https://pixhawk.ethz.ch/px4/dev/debug_values
#MODULES += examples/px4_mavlink_debug
# Tutorial code from
# https://pixhawk.ethz.ch/px4/dev/example_fixedwing_control
#MODULES += examples/fixedwing_control
# Hardware test
#MODULES += examples/hwtest
#
# Transitional support - add commands from the NuttX export archive.
#
# In general, these should move to modules over time.
#
# Each entry here is <command>.<priority>.<stacksize>.<entrypoint> but we use a helper macro
# to make the table a bit more readable.
#
define _B
$(strip $1).$(or $(strip $2),SCHED_PRIORITY_DEFAULT).$(or $(strip $3),CONFIG_PTHREAD_STACK_DEFAULT).$(strip $4)
endef
BUILTIN_COMMANDS := \
$(call _B, hello, , 2048, hello_main) \
$(call _B, i2c, , 2048, i2c_main)
+2 -2
View File
@@ -55,8 +55,8 @@ MODULES += systemcmds/top
MODULES += systemcmds/tests
MODULES += systemcmds/config
MODULES += systemcmds/nshterm
MODULES += systemcmds/hw_ver
MODULES += systemcmds/dumpfile
MODULES += systemcmds/ver
#
# General system control
@@ -70,7 +70,7 @@ MODULES += modules/gpio_led
# Estimation modules (EKF/ SO3 / other filters)
#
MODULES += modules/attitude_estimator_ekf
MODULES += modules/fw_att_pos_estimator
MODULES += modules/ekf_att_pos_estimator
MODULES += modules/position_estimator_inav
#MODULES += examples/flow_position_estimator
+2 -2
View File
@@ -64,8 +64,8 @@ MODULES += systemcmds/tests
MODULES += systemcmds/config
MODULES += systemcmds/nshterm
MODULES += systemcmds/mtd
MODULES += systemcmds/hw_ver
MODULES += systemcmds/dumpfile
MODULES += systemcmds/ver
#
# General system control
@@ -80,7 +80,7 @@ MODULES += modules/gpio_led
#
MODULES += modules/attitude_estimator_ekf
MODULES += modules/attitude_estimator_so3
MODULES += modules/fw_att_pos_estimator
MODULES += modules/ekf_att_pos_estimator
MODULES += modules/position_estimator_inav
MODULES += examples/flow_position_estimator
+1 -1
View File
@@ -30,7 +30,7 @@ MODULES += systemcmds/reboot
MODULES += systemcmds/tests
MODULES += systemcmds/nshterm
MODULES += systemcmds/mtd
MODULES += systemcmds/hw_ver
MODULES += systemcmds/ver
#
# Library modules
+4 -2
View File
@@ -113,7 +113,7 @@ endif
$(info % GIT_DESC = $(GIT_DESC))
#
# Set a default target so that included makefiles or errors here don't
# Set a default target so that included makefiles or errors here don't
# cause confusion.
#
# XXX We could do something cute here with $(DEFAULT_GOAL) if it's not one
@@ -177,7 +177,7 @@ GLOBAL_DEPS += $(MAKEFILE_LIST)
#
# Extra things we should clean
#
EXTRA_CLEANS =
EXTRA_CLEANS =
#
@@ -371,6 +371,8 @@ $(ROMFS_IMG): $(ROMFS_SCRATCH) $(ROMFS_DEPS) $(GLOBAL_DEPS)
$(ROMFS_SCRATCH): $(ROMFS_DEPS) $(GLOBAL_DEPS)
$(Q) $(MKDIR) -p $(ROMFS_SCRATCH)
$(Q) $(COPYDIR) $(ROMFS_ROOT)/* $(ROMFS_SCRATCH)
# delete all files in ROMFS_SCRATCH which start with a . or end with a ~
$(Q) $(RM) $(ROMFS_SCRATCH)/*/.[!.]* $(ROMFS_SCRATCH)/*/*~
ifneq ($(ROMFS_EXTRA_FILES),)
$(Q) $(MKDIR) -p $(ROMFS_SCRATCH)/extras
$(Q) $(COPY) $(ROMFS_EXTRA_FILES) $(ROMFS_SCRATCH)/extras
+12 -2
View File
@@ -48,6 +48,16 @@ NM = $(CROSSDEV)nm
OBJCOPY = $(CROSSDEV)objcopy
OBJDUMP = $(CROSSDEV)objdump
# Check if the right version of the toolchain is available
#
CROSSDEV_VER_SUPPORTED = 4.7
CROSSDEV_VER_FOUND = $(shell $(CC) -dumpversion)
ifeq (,$(findstring $(CROSSDEV_VER_SUPPORTED),$(CROSSDEV_VER_FOUND)))
$(error Unsupported version of $(CC), found: $(CROSSDEV_VER_FOUND) instead of $(CROSSDEV_VER_SUPPORTED).x)
endif
# XXX this is pulled pretty directly from the fmu Make.defs - needs cleanup
MAXOPTIMIZATION ?= -O3
@@ -76,7 +86,7 @@ ARCHINSTRUMENTATIONDEFINES_CORTEXM4F = -finstrument-functions \
ARCHINSTRUMENTATIONDEFINES_CORTEXM4 = -finstrument-functions \
-ffixed-r10
ARCHINSTRUMENTATIONDEFINES_CORTEXM3 =
ARCHINSTRUMENTATIONDEFINES_CORTEXM3 =
# Pick the right set of flags for the architecture.
#
@@ -265,7 +275,7 @@ define SYM_TO_BIN
$(Q) $(OBJCOPY) -O binary $1 $2
endef
# Take the raw binary $1 and make it into an object file $2.
# Take the raw binary $1 and make it into an object file $2.
# The symbol $3 points to the beginning of the file, and $3_len
# gives its length.
#
+263
View File
@@ -0,0 +1,263 @@
/************************************************************************************
* configs/aerocore/include/board.h
* include/arch/board/board.h
*
* Copyright (C) 2009 Gregory Nutt. All rights reserved.
* Author: Gregory Nutt <gnutt@nuttx.org>
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name NuttX nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
************************************************************************************/
#ifndef __ARCH_BOARD_BOARD_H
#define __ARCH_BOARD_BOARD_H
/************************************************************************************
* Included Files
************************************************************************************/
#include <nuttx/config.h>
#ifndef __ASSEMBLY__
# include <stdint.h>
#endif
#include <stm32.h>
/************************************************************************************
* Definitions
************************************************************************************/
/* Clocking *************************************************************************/
/* The AeroCore uses a 24MHz crystal connected to the HSE.
*
* This is the "standard" configuration as set up by arch/arm/src/stm32f40xx_rcc.c:
* System Clock source : PLL (HSE)
* SYSCLK(Hz) : 168000000 Determined by PLL configuration
* HCLK(Hz) : 168000000 (STM32_RCC_CFGR_HPRE)
* AHB Prescaler : 1 (STM32_RCC_CFGR_HPRE)
* APB1 Prescaler : 4 (STM32_RCC_CFGR_PPRE1)
* APB2 Prescaler : 2 (STM32_RCC_CFGR_PPRE2)
* HSE Frequency(Hz) : 24000000 (STM32_BOARD_XTAL)
* PLLM : 24 (STM32_PLLCFG_PLLM)
* PLLN : 336 (STM32_PLLCFG_PLLN)
* PLLP : 2 (STM32_PLLCFG_PLLP)
* PLLQ : 7 (STM32_PLLCFG_PPQ)
* Main regulator output voltage : Scale1 mode Needed for high speed SYSCLK
* Flash Latency(WS) : 5
* Prefetch Buffer : OFF
* Instruction cache : ON
* Data cache : ON
* Require 48MHz for USB OTG FS, : Enabled
* SDIO and RNG clock
*/
/* HSI - 16 MHz RC factory-trimmed
* LSI - 32 KHz RC
* HSE - On-board crystal frequency is 24MHz
* LSE - not installed
*/
#define STM32_BOARD_XTAL 24000000ul
#define STM32_HSI_FREQUENCY 16000000ul
#define STM32_LSI_FREQUENCY 32000
#define STM32_HSE_FREQUENCY STM32_BOARD_XTAL
/* Main PLL Configuration.
*
* PLL source is HSE
* PLL_VCO = (STM32_HSE_FREQUENCY / PLLM) * PLLN
* = (24,000,000 / 24) * 336
* = 336,000,000
* SYSCLK = PLL_VCO / PLLP
* = 336,000,000 / 2 = 168,000,000
* USB OTG FS, SDIO and RNG Clock
* = PLL_VCO / PLLQ
* = 48,000,000
*/
#define STM32_PLLCFG_PLLM RCC_PLLCFG_PLLM(24)
#define STM32_PLLCFG_PLLN RCC_PLLCFG_PLLN(336)
#define STM32_PLLCFG_PLLP RCC_PLLCFG_PLLP_2
#define STM32_PLLCFG_PLLQ RCC_PLLCFG_PLLQ(7)
#define STM32_SYSCLK_FREQUENCY 168000000ul
/* AHB clock (HCLK) is SYSCLK (168MHz) */
#define STM32_RCC_CFGR_HPRE RCC_CFGR_HPRE_SYSCLK /* HCLK = SYSCLK / 1 */
#define STM32_HCLK_FREQUENCY STM32_SYSCLK_FREQUENCY
#define STM32_BOARD_HCLK STM32_HCLK_FREQUENCY /* same as above, to satisfy compiler */
/* APB1 clock (PCLK1) is HCLK/4 (42MHz) */
#define STM32_RCC_CFGR_PPRE1 RCC_CFGR_PPRE1_HCLKd4 /* PCLK1 = HCLK / 4 */
#define STM32_PCLK1_FREQUENCY (STM32_HCLK_FREQUENCY/4)
/* Timers driven from APB1 will be twice PCLK1 */
#define STM32_APB1_TIM2_CLKIN (2*STM32_PCLK1_FREQUENCY)
#define STM32_APB1_TIM3_CLKIN (2*STM32_PCLK1_FREQUENCY)
#define STM32_APB1_TIM4_CLKIN (2*STM32_PCLK1_FREQUENCY)
#define STM32_APB1_TIM5_CLKIN (2*STM32_PCLK1_FREQUENCY)
#define STM32_APB1_TIM6_CLKIN (2*STM32_PCLK1_FREQUENCY)
#define STM32_APB1_TIM7_CLKIN (2*STM32_PCLK1_FREQUENCY)
#define STM32_APB1_TIM12_CLKIN (2*STM32_PCLK1_FREQUENCY)
#define STM32_APB1_TIM13_CLKIN (2*STM32_PCLK1_FREQUENCY)
#define STM32_APB1_TIM14_CLKIN (2*STM32_PCLK1_FREQUENCY)
/* APB2 clock (PCLK2) is HCLK/2 (84MHz) */
#define STM32_RCC_CFGR_PPRE2 RCC_CFGR_PPRE2_HCLKd2 /* PCLK2 = HCLK / 2 */
#define STM32_PCLK2_FREQUENCY (STM32_HCLK_FREQUENCY/2)
/* Timers driven from APB2 will be twice PCLK2 */
#define STM32_APB2_TIM1_CLKIN (2*STM32_PCLK2_FREQUENCY)
#define STM32_APB2_TIM8_CLKIN (2*STM32_PCLK2_FREQUENCY)
#define STM32_APB2_TIM9_CLKIN (2*STM32_PCLK2_FREQUENCY)
#define STM32_APB2_TIM10_CLKIN (2*STM32_PCLK2_FREQUENCY)
#define STM32_APB2_TIM11_CLKIN (2*STM32_PCLK2_FREQUENCY)
/* Timer Frequencies, if APBx is set to 1, frequency is same to APBx
* otherwise frequency is 2xAPBx.
* Note: TIM1,8 are on APB2, others on APB1
*/
#define STM32_TIM18_FREQUENCY (2*STM32_PCLK2_FREQUENCY)
#define STM32_TIM27_FREQUENCY (2*STM32_PCLK1_FREQUENCY)
/* Alternate function pin selections ************************************************/
/*
* UARTs.
*/
/* USART1 on PB[6,7]: GPS */
#define GPIO_USART1_RX GPIO_USART1_RX_2
#define GPIO_USART1_TX GPIO_USART1_TX_2
/* USART2 on PD[5,6]: J5 Breakout */
#define GPIO_USART2_RX GPIO_USART2_RX_2
#define GPIO_USART2_TX GPIO_USART2_TX_2
#define GPIO_USART2_CTS 0 // unused
#define GPIO_USART2_RTS 0 // unused
/* USART3 on PD[8,9]: to DuoVero UART2 */
#define GPIO_USART3_RX GPIO_USART3_RX_3
#define GPIO_USART3_TX GPIO_USART3_TX_3
#define GPIO_USART3_CTS 0 // unused
#define GPIO_USART3_RTS 0 // unused
/* UART7 on PE[78]: J7 Breakout */
#define GPIO_UART7_RX GPIO_UART7_RX_1
#define GPIO_UART7_TX GPIO_UART7_TX_1
/*
* UART8 on PE[0-1]: System Console on Port C of USB (J7)
* No alternate pin config
*/
/* USART[1,6] require a RX DMA configuration */
#define DMAMAP_USART1_RX DMAMAP_USART1_RX_2
#define DMAMAP_USART6_RX DMAMAP_USART6_RX_2
/*
* I2C
*
* The optional _GPIO configurations allow the I2C driver to manually
* reset the bus to clear stuck slaves. They match the pin configuration,
* but are normally-high GPIOs.
*/
/* PB[10-11]: I2C2 is broken out on J9 header */
#define GPIO_I2C2_SCL GPIO_I2C2_SCL_1
#define GPIO_I2C2_SDA GPIO_I2C2_SDA_1
#define GPIO_I2C2_SCL_GPIO (GPIO_OUTPUT|GPIO_OPENDRAIN|GPIO_SPEED_50MHz|GPIO_OUTPUT_SET|GPIO_PORTB|GPIO_PIN10)
#define GPIO_I2C2_SDA_GPIO (GPIO_OUTPUT|GPIO_OPENDRAIN|GPIO_SPEED_50MHz|GPIO_OUTPUT_SET|GPIO_PORTB|GPIO_PIN11)
/*
* SPI
*/
/* PA[4-7] SPI1 broken out on J12 */
#define GPIO_SPI1_NSS (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_SET|GPIO_PORTA|GPIO_PIN4) /* should be GPIO_SPI1_NSS_2 but use as a GPIO */
#define GPIO_SPI1_SCK (GPIO_SPI1_SCK_1|GPIO_SPEED_50MHz)
#define GPIO_SPI1_MISO (GPIO_SPI1_MISO_1|GPIO_SPEED_50MHz)
#define GPIO_SPI1_MOSI (GPIO_SPI1_MOSI_1|GPIO_SPEED_50MHz)
/* PB[12-15]: SPI2 connected to DuoVero SPI1 */
#define GPIO_SPI2_NSS (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_SET|GPIO_PORTB|GPIO_PIN9) /* should be GPIO_SPI2_NSS_2 but use as a GPIO */
#define GPIO_SPI2_SCK (GPIO_SPI2_SCK_2|GPIO_SPEED_50MHz)
#define GPIO_SPI2_MISO (GPIO_SPI2_MISO_1|GPIO_SPEED_50MHz)
#define GPIO_SPI2_MOSI (GPIO_SPI2_MOSI_1|GPIO_SPEED_50MHz)
/* PC[10-12]: SPI3 connected to onboard sensors */
#define GPIO_SPI3_SCK (GPIO_SPI3_SCK_2|GPIO_SPEED_50MHz)
#define GPIO_SPI3_MISO (GPIO_SPI3_MISO_2|GPIO_SPEED_50MHz)
#define GPIO_SPI3_MOSI (GPIO_SPI3_MOSI_2|GPIO_SPEED_50MHz)
/* PE[11-14]: SPI4 connected to FRAM */
#define GPIO_SPI4_NSS (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_SET|GPIO_PORTE|GPIO_PIN11) /* should be GPIO_SPI4_NSS_2 but use as a GPIO */
#define GPIO_SPI4_SCK (GPIO_SPI4_SCK_2|GPIO_SPEED_50MHz)
#define GPIO_SPI4_MISO (GPIO_SPI4_MISO_2|GPIO_SPEED_50MHz)
#define GPIO_SPI4_MOSI (GPIO_SPI4_MOSI_2|GPIO_SPEED_50MHz)
/************************************************************************************
* Public Data
************************************************************************************/
#ifndef __ASSEMBLY__
#undef EXTERN
#if defined(__cplusplus)
#define EXTERN extern "C"
extern "C" {
#else
#define EXTERN extern
#endif
/************************************************************************************
* Public Function Prototypes
************************************************************************************/
/************************************************************************************
* Name: stm32_boardinitialize
*
* Description:
* All STM32 architectures must provide the following entry point. This entry point
* is called early in the intitialization -- after all memory has been configured
* and mapped but before any devices have been initialized.
*
************************************************************************************/
EXTERN void stm32_boardinitialize(void);
#undef EXTERN
#if defined(__cplusplus)
}
#endif
#endif /* __ASSEMBLY__ */
#endif /* __ARCH_BOARD_BOARD_H */
@@ -1,8 +1,6 @@
/****************************************************************************
*
* Copyright (C) 2012 PX4 Development Team. All rights reserved.
* Author: @author Thomas Gubler <thomasgubler@student.ethz.ch>
*
* Copyright (C) 2013 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
@@ -33,16 +31,12 @@
*
****************************************************************************/
/* @file Fixed Wing Attitude Rate Control */
/**
* nsh_romfsetc.h
*
* This file is a stub for 'make export' purposes; the actual ROMFS
* must be supplied by the library client.
*/
#ifndef FIXEDWING_ATT_CONTROL_RATE_H_
#define FIXEDWING_ATT_CONTROL_RATE_H_
#include <uORB/topics/vehicle_rates_setpoint.h>
#include <uORB/topics/actuator_controls.h>
int fixedwing_att_control_rates(const struct vehicle_rates_setpoint_s *rate_sp,
const float rates[],
struct actuator_controls_s *actuators);
#endif /* FIXEDWING_ATT_CONTROL_RATE_H_ */
extern unsigned char romfs_img[];
extern unsigned int romfs_img_len;
+179
View File
@@ -0,0 +1,179 @@
############################################################################
# configs/aerocore/nsh/Make.defs
#
# Copyright (C) 2011 Gregory Nutt. All rights reserved.
# Author: Gregory Nutt <gnutt@nuttx.org>
#
# Redistribution and use in source and binary forms, with or without
# modification, are permitted provided that the following conditions
# are met:
#
# 1. Redistributions of source code must retain the above copyright
# notice, this list of conditions and the following disclaimer.
# 2. Redistributions in binary form must reproduce the above copyright
# notice, this list of conditions and the following disclaimer in
# the documentation and/or other materials provided with the
# distribution.
# 3. Neither the name NuttX nor the names of its contributors may be
# used to endorse or promote products derived from this software
# without specific prior written permission.
#
# THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
# "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
# LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
# FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
# COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
# INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
# BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
# OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
# AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
# LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
# ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
# POSSIBILITY OF SUCH DAMAGE.
#
############################################################################
include ${TOPDIR}/.config
include ${TOPDIR}/tools/Config.mk
#
# We only support building with the ARM bare-metal toolchain from
# https://launchpad.net/gcc-arm-embedded on Windows, Linux or Mac OS.
#
CONFIG_ARMV7M_TOOLCHAIN := GNU_EABI
include ${TOPDIR}/arch/arm/src/armv7-m/Toolchain.defs
CC = $(CROSSDEV)gcc
CXX = $(CROSSDEV)g++
CPP = $(CROSSDEV)gcc -E
LD = $(CROSSDEV)ld
AR = $(CROSSDEV)ar rcs
NM = $(CROSSDEV)nm
OBJCOPY = $(CROSSDEV)objcopy
OBJDUMP = $(CROSSDEV)objdump
MAXOPTIMIZATION = -O3
ARCHCPUFLAGS = -mcpu=cortex-m4 \
-mthumb \
-march=armv7e-m \
-mfpu=fpv4-sp-d16 \
-mfloat-abi=hard
# enable precise stack overflow tracking
INSTRUMENTATIONDEFINES = -finstrument-functions \
-ffixed-r10
# pull in *just* libm from the toolchain ... this is grody
LIBM = "${shell $(CC) $(ARCHCPUFLAGS) -print-file-name=libm.a}"
EXTRA_LIBS += $(LIBM)
# use our linker script
LDSCRIPT = ld.script
ifeq ($(WINTOOL),y)
# Windows-native toolchains
DIRLINK = $(TOPDIR)/tools/copydir.sh
DIRUNLINK = $(TOPDIR)/tools/unlink.sh
MKDEP = $(TOPDIR)/tools/mknulldeps.sh
ARCHINCLUDES = -I. -isystem "${shell cygpath -w $(TOPDIR)/include}"
ARCHXXINCLUDES = -I. -isystem "${shell cygpath -w $(TOPDIR)/include}" -isystem "${shell cygpath -w $(TOPDIR)/include/cxx}"
ARCHSCRIPT = -T "${shell cygpath -w $(TOPDIR)/configs/$(CONFIG_ARCH_BOARD)/scripts/$(LDSCRIPT)}"
else
ifeq ($(PX4_WINTOOL),y)
# Windows-native toolchains (MSYS)
DIRLINK = $(TOPDIR)/tools/copydir.sh
DIRUNLINK = $(TOPDIR)/tools/unlink.sh
MKDEP = $(TOPDIR)/tools/mknulldeps.sh
ARCHINCLUDES = -I. -isystem $(TOPDIR)/include
ARCHXXINCLUDES = -I. -isystem $(TOPDIR)/include -isystem $(TOPDIR)/include/cxx
ARCHSCRIPT = -T$(TOPDIR)/configs/$(CONFIG_ARCH_BOARD)/scripts/$(LDSCRIPT)
else
# Linux/Cygwin-native toolchain
MKDEP = $(TOPDIR)/tools/mkdeps.sh
ARCHINCLUDES = -I. -isystem $(TOPDIR)/include
ARCHXXINCLUDES = -I. -isystem $(TOPDIR)/include -isystem $(TOPDIR)/include/cxx
ARCHSCRIPT = -T$(TOPDIR)/configs/$(CONFIG_ARCH_BOARD)/scripts/$(LDSCRIPT)
endif
endif
# tool versions
ARCHCCVERSION = ${shell $(CC) -v 2>&1 | sed -n '/^gcc version/p' | sed -e 's/^gcc version \([0-9\.]\)/\1/g' -e 's/[-\ ].*//g' -e '1q'}
ARCHCCMAJOR = ${shell echo $(ARCHCCVERSION) | cut -d'.' -f1}
# optimisation flags
ARCHOPTIMIZATION = $(MAXOPTIMIZATION) \
-fno-strict-aliasing \
-fno-strength-reduce \
-fomit-frame-pointer \
-funsafe-math-optimizations \
-fno-builtin-printf \
-ffunction-sections \
-fdata-sections
ifeq ("${CONFIG_DEBUG_SYMBOLS}","y")
ARCHOPTIMIZATION += -g
endif
ARCHCFLAGS = -std=gnu99
ARCHCXXFLAGS = -fno-exceptions -fno-rtti -std=gnu++0x
ARCHWARNINGS = -Wall \
-Wextra \
-Wdouble-promotion \
-Wshadow \
-Wfloat-equal \
-Wframe-larger-than=1024 \
-Wpointer-arith \
-Wlogical-op \
-Wmissing-declarations \
-Wpacked \
-Wno-unused-parameter
# -Wcast-qual - generates spurious noreturn attribute warnings, try again later
# -Wconversion - would be nice, but too many "risky-but-safe" conversions in the code
# -Wcast-align - would help catch bad casts in some cases, but generates too many false positives
ARCHCWARNINGS = $(ARCHWARNINGS) \
-Wbad-function-cast \
-Wstrict-prototypes \
-Wold-style-declaration \
-Wmissing-parameter-type \
-Wmissing-prototypes \
-Wnested-externs \
-Wunsuffixed-float-constants
ARCHWARNINGSXX = $(ARCHWARNINGS) \
-Wno-psabi
ARCHDEFINES =
ARCHPICFLAGS = -fpic -msingle-pic-base -mpic-register=r10
# this seems to be the only way to add linker flags
EXTRA_LIBS += --warn-common \
--gc-sections
CFLAGS = $(ARCHCFLAGS) $(ARCHCWARNINGS) $(ARCHOPTIMIZATION) $(ARCHCPUFLAGS) $(ARCHINCLUDES) $(INSTRUMENTATIONDEFINES) $(ARCHDEFINES) $(EXTRADEFINES) -pipe -fno-common
CPICFLAGS = $(ARCHPICFLAGS) $(CFLAGS)
CXXFLAGS = $(ARCHCXXFLAGS) $(ARCHWARNINGSXX) $(ARCHOPTIMIZATION) $(ARCHCPUFLAGS) $(ARCHXXINCLUDES) $(INSTRUMENTATIONDEFINES) $(ARCHDEFINES) $(EXTRADEFINES) -pipe
CXXPICFLAGS = $(ARCHPICFLAGS) $(CXXFLAGS)
CPPFLAGS = $(ARCHINCLUDES) $(INSTRUMENTATIONDEFINES) $(ARCHDEFINES) $(EXTRADEFINES)
AFLAGS = $(CFLAGS) -D__ASSEMBLY__
NXFLATLDFLAGS1 = -r -d -warn-common
NXFLATLDFLAGS2 = $(NXFLATLDFLAGS1) -T$(TOPDIR)/binfmt/libnxflat/gnu-nxflat.ld -no-check-sections
LDNXFLATFLAGS = -e main -s 2048
OBJEXT = .o
LIBEXT = .a
EXEEXT =
# produce partially-linked $1 from files in $2
define PRELINK
@echo "PRELINK: $1"
$(Q) $(LD) -Ur -o $1 $2 && $(OBJCOPY) --localize-hidden $1
endef
HOSTCC = gcc
HOSTINCLUDES = -I.
HOSTCFLAGS = -Wall -Wstrict-prototypes -Wshadow -g -pipe
HOSTLDFLAGS =
@@ -1,6 +1,8 @@
############################################################################
# configs/aerocore/nsh/appconfig
#
# Copyright (c) 2012, 2013 PX4 Development Team. All rights reserved.
# Copyright (C) 2011 Gregory Nutt. All rights reserved.
# Author: Gregory Nutt <gnutt@nuttx.org>
#
# Redistribution and use in source and binary forms, with or without
# modification, are permitted provided that the following conditions
@@ -12,7 +14,7 @@
# notice, this list of conditions and the following disclaimer in
# the documentation and/or other materials provided with the
# distribution.
# 3. Neither the name PX4 nor the names of its contributors may be
# 3. Neither the name NuttX nor the names of its contributors may be
# used to endorse or promote products derived from this software
# without specific prior written permission.
#
@@ -31,12 +33,10 @@
#
############################################################################
#
# Full attitude / position Extended Kalman Filter
#
# Path to example in apps/examples containing the user_start entry point
MODULE_COMMAND = att_pos_estimator_ekf
CONFIGURED_APPS += examples/nsh
SRCS = kalman_main.cpp \
KalmanNav.cpp \
params.c
# The NSH application library
CONFIGURED_APPS += nshlib
CONFIGURED_APPS += system/readline
File diff suppressed because it is too large Load Diff
@@ -1,6 +1,8 @@
############################################################################
#!/bin/bash
# configs/aerocore/nsh/setenv.sh
#
# Copyright (c) 2012, 2013 PX4 Development Team. All rights reserved.
# Copyright (C) 2011 Gregory Nutt. All rights reserved.
# Author: Gregory Nutt <gnutt@nuttx.org>
#
# Redistribution and use in source and binary forms, with or without
# modification, are permitted provided that the following conditions
@@ -12,7 +14,7 @@
# notice, this list of conditions and the following disclaimer in
# the documentation and/or other materials provided with the
# distribution.
# 3. Neither the name PX4 nor the names of its contributors may be
# 3. Neither the name NuttX nor the names of its contributors may be
# used to endorse or promote products derived from this software
# without specific prior written permission.
#
@@ -29,12 +31,37 @@
# ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
# POSSIBILITY OF SUCH DAMAGE.
#
############################################################################
#
# Fixedwing PositionControl application
#
if [ "$_" = "$0" ] ; then
echo "You must source this script, not run it!" 1>&2
exit 1
fi
MODULE_COMMAND = fixedwing_pos_control
WD=`pwd`
if [ ! -x "setenv.sh" ]; then
echo "This script must be executed from the top-level NuttX build directory"
exit 1
fi
SRCS = fixedwing_pos_control_main.c
if [ -z "${PATH_ORIG}" ]; then
export PATH_ORIG="${PATH}"
fi
# This the Cygwin path to the location where I installed the RIDE
# toolchain under windows. You will also have to edit this if you install
# the RIDE toolchain in any other location
#export TOOLCHAIN_BIN="/cygdrive/c/Program Files (x86)/Raisonance/Ride/arm-gcc/bin"
# This the Cygwin path to the location where I installed the CodeSourcery
# toolchain under windows. You will also have to edit this if you install
# the CodeSourcery toolchain in any other location
export TOOLCHAIN_BIN="/cygdrive/c/Program Files (x86)/CodeSourcery/Sourcery G++ Lite/bin"
# This the Cygwin path to the location where I build the buildroot
# toolchain.
#export TOOLCHAIN_BIN="${WD}/../misc/buildroot/build_arm_nofpu/staging_dir/bin"
# Add the path to the toolchain to the PATH varialble
export PATH="${TOOLCHAIN_BIN}:/sbin:/usr/sbin:${PATH_ORIG}"
echo "PATH : ${PATH}"
+150
View File
@@ -0,0 +1,150 @@
/****************************************************************************
* configs/aerocore/common/ld.script
*
* Copyright (C) 2011 Gregory Nutt. All rights reserved.
* Author: Gregory Nutt <gnutt@nuttx.org>
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name NuttX nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
/* The STM32F427 has 2048Kb of FLASH beginning at address 0x0800:0000 and
* 256Kb of SRAM. SRAM is split up into three blocks:
*
* 1) 112Kb of SRAM beginning at address 0x2000:0000
* 2) 16Kb of SRAM beginning at address 0x2001:c000
* 3) 64Kb of SRAM beginning at address 0x2002:0000
* 4) 64Kb of TCM SRAM beginning at address 0x1000:0000
*
* When booting from FLASH, FLASH memory is aliased to address 0x0000:0000
* where the code expects to begin execution by jumping to the entry point in
* the 0x0800:0000 address range.
*
* The first 0x4000 of flash is reserved for the bootloader.
*/
MEMORY
{
flash (rx) : ORIGIN = 0x08004000, LENGTH = 2032K
sram (rwx) : ORIGIN = 0x20000000, LENGTH = 192K
ccsram (rwx) : ORIGIN = 0x10000000, LENGTH = 64K
}
OUTPUT_ARCH(arm)
ENTRY(__start) /* treat __start as the anchor for dead code stripping */
EXTERN(_vectors) /* force the vectors to be included in the output */
/*
* Ensure that abort() is present in the final object. The exception handling
* code pulled in by libgcc.a requires it (and that code cannot be easily avoided).
*/
EXTERN(abort)
SECTIONS
{
.text : {
_stext = ABSOLUTE(.);
*(.vectors)
*(.text .text.*)
*(.fixup)
*(.gnu.warning)
*(.rodata .rodata.*)
*(.gnu.linkonce.t.*)
*(.got)
*(.gcc_except_table)
*(.gnu.linkonce.r.*)
_etext = ABSOLUTE(.);
/*
* This is a hack to make the newlib libm __errno() call
* use the NuttX get_errno_ptr() function.
*/
__errno = get_errno_ptr;
} > flash
/*
* Init functions (static constructors and the like)
*/
.init_section : {
_sinit = ABSOLUTE(.);
KEEP(*(.init_array .init_array.*))
_einit = ABSOLUTE(.);
} > flash
/*
* Construction data for parameters.
*/
__param ALIGN(4): {
__param_start = ABSOLUTE(.);
KEEP(*(__param*))
__param_end = ABSOLUTE(.);
} > flash
.ARM.extab : {
*(.ARM.extab*)
} > flash
__exidx_start = ABSOLUTE(.);
.ARM.exidx : {
*(.ARM.exidx*)
} > flash
__exidx_end = ABSOLUTE(.);
_eronly = ABSOLUTE(.);
.data : {
_sdata = ABSOLUTE(.);
*(.data .data.*)
*(.gnu.linkonce.d.*)
CONSTRUCTORS
_edata = ABSOLUTE(.);
} > sram AT > flash
.bss : {
_sbss = ABSOLUTE(.);
*(.bss .bss.*)
*(.gnu.linkonce.b.*)
*(COMMON)
_ebss = ABSOLUTE(.);
} > sram
/* Stabs debugging sections. */
.stab 0 : { *(.stab) }
.stabstr 0 : { *(.stabstr) }
.stab.excl 0 : { *(.stab.excl) }
.stab.exclstr 0 : { *(.stab.exclstr) }
.stab.index 0 : { *(.stab.index) }
.stab.indexstr 0 : { *(.stab.indexstr) }
.comment 0 : { *(.comment) }
.debug_abbrev 0 : { *(.debug_abbrev) }
.debug_info 0 : { *(.debug_info) }
.debug_line 0 : { *(.debug_line) }
.debug_pubnames 0 : { *(.debug_pubnames) }
.debug_aranges 0 : { *(.debug_aranges) }
}
@@ -1,6 +1,8 @@
############################################################################
# configs/aerocore/src/Makefile
#
# Copyright (c) 2012, 2013 PX4 Development Team. All rights reserved.
# Copyright (C) 2011 Gregory Nutt. All rights reserved.
# Author: Gregory Nutt <gnutt@nuttx.org>
#
# Redistribution and use in source and binary forms, with or without
# modification, are permitted provided that the following conditions
@@ -12,7 +14,7 @@
# notice, this list of conditions and the following disclaimer in
# the documentation and/or other materials provided with the
# distribution.
# 3. Neither the name PX4 nor the names of its contributors may be
# 3. Neither the name NuttX nor the names of its contributors may be
# used to endorse or promote products derived from this software
# without specific prior written permission.
#
@@ -31,14 +33,52 @@
#
############################################################################
#
# Makefile to build the position estimator
#
-include $(TOPDIR)/Make.defs
MODULE_COMMAND = position_estimator
CFLAGS += -I$(TOPDIR)/sched
# XXX this should be converted to a deamon, its a pretty bad example app
MODULE_PRIORITY = SCHED_PRIORITY_DEFAULT
MODULE_STACKSIZE = 4096
ASRCS =
AOBJS = $(ASRCS:.S=$(OBJEXT))
CSRCS = empty.c
COBJS = $(CSRCS:.c=$(OBJEXT))
SRCS = $(ASRCS) $(CSRCS)
OBJS = $(AOBJS) $(COBJS)
ARCH_SRCDIR = $(TOPDIR)/arch/$(CONFIG_ARCH)/src
ifeq ($(WINTOOL),y)
CFLAGS += -I "${shell cygpath -w $(ARCH_SRCDIR)/chip}" \
-I "${shell cygpath -w $(ARCH_SRCDIR)/common}" \
-I "${shell cygpath -w $(ARCH_SRCDIR)/armv7-m}"
else
CFLAGS += -I$(ARCH_SRCDIR)/chip -I$(ARCH_SRCDIR)/common -I$(ARCH_SRCDIR)/armv7-m
endif
all: libboard$(LIBEXT)
$(AOBJS): %$(OBJEXT): %.S
$(call ASSEMBLE, $<, $@)
$(COBJS) $(LINKOBJS): %$(OBJEXT): %.c
$(call COMPILE, $<, $@)
libboard$(LIBEXT): $(OBJS)
$(call ARCHIVE, $@, $(OBJS))
.depend: Makefile $(SRCS)
$(Q) $(MKDEP) $(CC) -- $(CFLAGS) -- $(SRCS) >Make.dep
$(Q) touch $@
depend: .depend
clean:
$(call DELFILE, libboard$(LIBEXT))
$(call CLEAN)
distclean: clean
$(call DELFILE, Make.dep)
$(call DELFILE, .depend)
-include Make.dep
SRCS = position_estimator_main.c
+4
View File
@@ -0,0 +1,4 @@
/*
* There are no source files here, but libboard.a can't be empty, so
* we have this empty source file to keep it company.
*/
+7 -7
View File
@@ -418,7 +418,7 @@ CONFIG_PREALLOC_TIMERS=50
# Stack and heap information
#
CONFIG_IDLETHREAD_STACKSIZE=4096
CONFIG_USERMAIN_STACKSIZE=4096
CONFIG_USERMAIN_STACKSIZE=3500
CONFIG_PTHREAD_STACK_MIN=512
CONFIG_PTHREAD_STACK_DEFAULT=2048
@@ -504,8 +504,8 @@ CONFIG_MTD_BYTE_WRITE=y
#
# USART1 Configuration
#
CONFIG_USART1_RXBUFSIZE=512
CONFIG_USART1_TXBUFSIZE=512
CONFIG_USART1_RXBUFSIZE=300
CONFIG_USART1_TXBUFSIZE=300
CONFIG_USART1_BAUD=57600
CONFIG_USART1_BITS=8
CONFIG_USART1_PARITY=0
@@ -528,8 +528,8 @@ CONFIG_USART2_OFLOWCONTROL=y
#
# UART5 Configuration
#
CONFIG_UART5_RXBUFSIZE=512
CONFIG_UART5_TXBUFSIZE=512
CONFIG_UART5_RXBUFSIZE=300
CONFIG_UART5_TXBUFSIZE=300
CONFIG_UART5_BAUD=57600
CONFIG_UART5_BITS=8
CONFIG_UART5_PARITY=0
@@ -540,8 +540,8 @@ CONFIG_UART5_2STOP=0
#
# USART6 Configuration
#
CONFIG_USART6_RXBUFSIZE=512
CONFIG_USART6_TXBUFSIZE=512
CONFIG_USART6_RXBUFSIZE=128
CONFIG_USART6_TXBUFSIZE=64
CONFIG_USART6_BAUD=57600
CONFIG_USART6_BITS=8
CONFIG_USART6_PARITY=0
+4
View File
@@ -268,6 +268,10 @@
#define GPIO_SPI2_MOSI (GPIO_SPI2_MOSI_1|GPIO_SPEED_50MHz)
#define GPIO_SPI2_SCK (GPIO_SPI2_SCK_2|GPIO_SPEED_50MHz)
#define GPIO_SPI4_MISO (GPIO_SPI4_MISO_1|GPIO_SPEED_50MHz)
#define GPIO_SPI4_MOSI (GPIO_SPI4_MOSI_1|GPIO_SPEED_50MHz)
#define GPIO_SPI4_SCK (GPIO_SPI4_SCK_1|GPIO_SPEED_50MHz)
/************************************************************************************
* Public Data
************************************************************************************/
+1 -1
View File
@@ -235,7 +235,7 @@ CONFIG_STM32_SDIO=y
CONFIG_STM32_SPI1=y
CONFIG_STM32_SPI2=y
# CONFIG_STM32_SPI3 is not set
# CONFIG_STM32_SPI4 is not set
CONFIG_STM32_SPI4=y
# CONFIG_STM32_SPI5 is not set
# CONFIG_STM32_SPI6 is not set
CONFIG_STM32_SYSCFG=y

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