mirror of
https://github.com/PX4/PX4-Autopilot.git
synced 2026-05-28 10:46:33 +08:00
Merge remote-tracking branch 'upstream/master' into hott_v2
This commit is contained in:
@@ -32,6 +32,7 @@ ROMFS_FSSPEC := $(SRCROOT)/scripts/rcS~init.d/rcS \
|
|||||||
$(SRCROOT)/mixers/FMU_RET.mix~mixers/FMU_ERT.mix \
|
$(SRCROOT)/mixers/FMU_RET.mix~mixers/FMU_ERT.mix \
|
||||||
$(SRCROOT)/mixers/FMU_quad_x.mix~mixers/FMU_quad_x.mix \
|
$(SRCROOT)/mixers/FMU_quad_x.mix~mixers/FMU_quad_x.mix \
|
||||||
$(SRCROOT)/mixers/FMU_quad_+.mix~mixers/FMU_quad_+.mix \
|
$(SRCROOT)/mixers/FMU_quad_+.mix~mixers/FMU_quad_+.mix \
|
||||||
|
$(SRCROOT)/mixers/FMU_quad_v.mix~mixers/FMU_quad_v.mix \
|
||||||
$(SRCROOT)/mixers/FMU_hex_x.mix~mixers/FMU_hex_x.mix \
|
$(SRCROOT)/mixers/FMU_hex_x.mix~mixers/FMU_hex_x.mix \
|
||||||
$(SRCROOT)/mixers/FMU_hex_+.mix~mixers/FMU_hex_+.mix \
|
$(SRCROOT)/mixers/FMU_hex_+.mix~mixers/FMU_hex_+.mix \
|
||||||
$(SRCROOT)/mixers/FMU_octo_x.mix~mixers/FMU_octo_x.mix \
|
$(SRCROOT)/mixers/FMU_octo_x.mix~mixers/FMU_octo_x.mix \
|
||||||
|
|||||||
@@ -0,0 +1,7 @@
|
|||||||
|
Multirotor mixer for PX4FMU
|
||||||
|
===========================
|
||||||
|
|
||||||
|
This file defines a single mixer for a quadrotor in the V configuration. All controls
|
||||||
|
are mixed 100%.
|
||||||
|
|
||||||
|
R: 4v 10000 10000 10000 0
|
||||||
@@ -35,8 +35,9 @@ APPNAME = attitude_estimator_ekf
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|||||||
PRIORITY = SCHED_PRIORITY_DEFAULT
|
PRIORITY = SCHED_PRIORITY_DEFAULT
|
||||||
STACKSIZE = 2048
|
STACKSIZE = 2048
|
||||||
|
|
||||||
CSRCS = attitude_estimator_ekf_main.c \
|
CXXSRCS = attitude_estimator_ekf_main.cpp
|
||||||
attitude_estimator_ekf_params.c \
|
|
||||||
|
CSRCS = attitude_estimator_ekf_params.c \
|
||||||
codegen/eye.c \
|
codegen/eye.c \
|
||||||
codegen/attitudeKalmanfilter.c \
|
codegen/attitudeKalmanfilter.c \
|
||||||
codegen/mrdivide.c \
|
codegen/mrdivide.c \
|
||||||
|
|||||||
+12
-5
@@ -66,11 +66,17 @@
|
|||||||
#include <systemlib/perf_counter.h>
|
#include <systemlib/perf_counter.h>
|
||||||
#include <systemlib/err.h>
|
#include <systemlib/err.h>
|
||||||
|
|
||||||
|
#ifdef __cplusplus
|
||||||
|
extern "C" {
|
||||||
|
#endif
|
||||||
#include "codegen/attitudeKalmanfilter_initialize.h"
|
#include "codegen/attitudeKalmanfilter_initialize.h"
|
||||||
#include "codegen/attitudeKalmanfilter.h"
|
#include "codegen/attitudeKalmanfilter.h"
|
||||||
#include "attitude_estimator_ekf_params.h"
|
#include "attitude_estimator_ekf_params.h"
|
||||||
|
#ifdef __cplusplus
|
||||||
|
}
|
||||||
|
#endif
|
||||||
|
|
||||||
__EXPORT int attitude_estimator_ekf_main(int argc, char *argv[]);
|
extern "C" __EXPORT int attitude_estimator_ekf_main(int argc, char *argv[]);
|
||||||
|
|
||||||
static bool thread_should_exit = false; /**< Deamon exit flag */
|
static bool thread_should_exit = false; /**< Deamon exit flag */
|
||||||
static bool thread_running = false; /**< Deamon status flag */
|
static bool thread_running = false; /**< Deamon status flag */
|
||||||
@@ -265,10 +271,11 @@ const unsigned int loop_interval_alarm = 6500; // loop interval in microseconds
|
|||||||
/* Main loop*/
|
/* Main loop*/
|
||||||
while (!thread_should_exit) {
|
while (!thread_should_exit) {
|
||||||
|
|
||||||
struct pollfd fds[2] = {
|
struct pollfd fds[2];
|
||||||
{ .fd = sub_raw, .events = POLLIN },
|
fds[0].fd = sub_raw;
|
||||||
{ .fd = sub_params, .events = POLLIN }
|
fds[0].events = POLLIN;
|
||||||
};
|
fds[1].fd = sub_params;
|
||||||
|
fds[1].events = POLLIN;
|
||||||
int ret = poll(fds, 2, 1000);
|
int ret = poll(fds, 2, 1000);
|
||||||
|
|
||||||
if (ret < 0) {
|
if (ret < 0) {
|
||||||
@@ -92,6 +92,7 @@
|
|||||||
|
|
||||||
#include <nuttx/config.h>
|
#include <nuttx/config.h>
|
||||||
|
|
||||||
|
#include <arch/board/board.h>
|
||||||
#include <drivers/device/i2c.h>
|
#include <drivers/device/i2c.h>
|
||||||
|
|
||||||
#include <sys/types.h>
|
#include <sys/types.h>
|
||||||
@@ -841,7 +842,7 @@ int
|
|||||||
blinkm_main(int argc, char *argv[])
|
blinkm_main(int argc, char *argv[])
|
||||||
{
|
{
|
||||||
|
|
||||||
int i2cdevice = 3;
|
int i2cdevice = PX4_I2C_BUS_EXPANSION;
|
||||||
int blinkmadr = 9;
|
int blinkmadr = 9;
|
||||||
|
|
||||||
int x;
|
int x;
|
||||||
|
|||||||
@@ -33,7 +33,14 @@
|
|||||||
*
|
*
|
||||||
****************************************************************************/
|
****************************************************************************/
|
||||||
|
|
||||||
/* @file U-Blox protocol implementation */
|
/**
|
||||||
|
* @file ubx.cpp
|
||||||
|
*
|
||||||
|
* U-Blox protocol implementation. Following u-blox 6/7 Receiver Description
|
||||||
|
* including Prototol Specification.
|
||||||
|
*
|
||||||
|
* @see http://www.u-blox.com/images/downloads/Product_Docs/u-blox6_ReceiverDescriptionProtocolSpec_%28GPS.G6-SW-10018%29.pdf
|
||||||
|
*/
|
||||||
|
|
||||||
#include <unistd.h>
|
#include <unistd.h>
|
||||||
#include <stdio.h>
|
#include <stdio.h>
|
||||||
@@ -633,16 +640,17 @@ UBX::handle_message()
|
|||||||
}
|
}
|
||||||
|
|
||||||
case NAV_VELNED: {
|
case NAV_VELNED: {
|
||||||
// printf("GOT NAV_VELNED MESSAGE\n");
|
|
||||||
|
|
||||||
if (!_waiting_for_ack) {
|
if (!_waiting_for_ack) {
|
||||||
|
/* 35.15 NAV-VELNED (0x01 0x12) message (page 181 / 210 of reference manual */
|
||||||
gps_bin_nav_velned_packet_t *packet = (gps_bin_nav_velned_packet_t *) _rx_buffer;
|
gps_bin_nav_velned_packet_t *packet = (gps_bin_nav_velned_packet_t *) _rx_buffer;
|
||||||
|
|
||||||
_gps_position->vel_m_s = (float)packet->speed * 1e-2f;
|
_gps_position->vel_m_s = (float)packet->speed * 1e-2f;
|
||||||
_gps_position->vel_n_m_s = (float)packet->velN * 1e-2f;
|
_gps_position->vel_n_m_s = (float)packet->velN * 1e-2f; /* NED NORTH velocity */
|
||||||
_gps_position->vel_e_m_s = (float)packet->velE * 1e-2f;
|
_gps_position->vel_e_m_s = (float)packet->velE * 1e-2f; /* NED EAST velocity */
|
||||||
_gps_position->vel_d_m_s = (float)packet->velD * 1e-2f;
|
_gps_position->vel_d_m_s = (float)packet->velD * 1e-2f; /* NED DOWN velocity */
|
||||||
_gps_position->cog_rad = (float)packet->heading * M_DEG_TO_RAD_F * 1e-5f;
|
_gps_position->cog_rad = (float)packet->heading * M_DEG_TO_RAD_F * 1e-5f;
|
||||||
|
_gps_position->c_variance_rad = (float)packet->cAcc * M_DEG_TO_RAD_F * 1e-5f;
|
||||||
_gps_position->vel_ned_valid = true;
|
_gps_position->vel_ned_valid = true;
|
||||||
_gps_position->timestamp_velocity = hrt_absolute_time();
|
_gps_position->timestamp_velocity = hrt_absolute_time();
|
||||||
}
|
}
|
||||||
|
|||||||
@@ -0,0 +1,44 @@
|
|||||||
|
############################################################################
|
||||||
|
#
|
||||||
|
# Copyright (C) 2012 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
|
||||||
|
# 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 PX4 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.
|
||||||
|
#
|
||||||
|
############################################################################
|
||||||
|
|
||||||
|
#
|
||||||
|
# Interface driver for the Mikrokopter BLCtrl
|
||||||
|
#
|
||||||
|
|
||||||
|
APPNAME = mkblctrl
|
||||||
|
PRIORITY = SCHED_PRIORITY_DEFAULT
|
||||||
|
STACKSIZE = 2048
|
||||||
|
|
||||||
|
INCLUDES = $(TOPDIR)/arch/arm/src/stm32 $(TOPDIR)/arch/arm/src/common
|
||||||
|
|
||||||
|
include $(APPDIR)/mk/app.mk
|
||||||
File diff suppressed because it is too large
Load Diff
@@ -125,7 +125,7 @@
|
|||||||
# define HRT_TIMER_VECTOR STM32_IRQ_TIM8CC
|
# define HRT_TIMER_VECTOR STM32_IRQ_TIM8CC
|
||||||
# define HRT_TIMER_CLOCK STM32_APB2_TIM8_CLKIN
|
# define HRT_TIMER_CLOCK STM32_APB2_TIM8_CLKIN
|
||||||
# if CONFIG_STM32_TIM8
|
# if CONFIG_STM32_TIM8
|
||||||
# error must not set CONFIG_STM32_TIM8=y and HRT_TIMER=6
|
# error must not set CONFIG_STM32_TIM8=y and HRT_TIMER=8
|
||||||
# endif
|
# endif
|
||||||
#elif HRT_TIMER == 9
|
#elif HRT_TIMER == 9
|
||||||
# define HRT_TIMER_BASE STM32_TIM9_BASE
|
# define HRT_TIMER_BASE STM32_TIM9_BASE
|
||||||
|
|||||||
@@ -494,7 +494,7 @@ ToneAlarm::init()
|
|||||||
return ret;
|
return ret;
|
||||||
|
|
||||||
/* configure the GPIO to the idle state */
|
/* configure the GPIO to the idle state */
|
||||||
stm32_configgpio(GPIO_TONE_ALARM);
|
stm32_configgpio(GPIO_TONE_ALARM_IDLE);
|
||||||
|
|
||||||
/* clock/power on our timer */
|
/* clock/power on our timer */
|
||||||
modifyreg32(STM32_RCC_APB1ENR, 0, TONE_ALARM_CLOCK_ENABLE);
|
modifyreg32(STM32_RCC_APB1ENR, 0, TONE_ALARM_CLOCK_ENABLE);
|
||||||
@@ -606,6 +606,8 @@ ToneAlarm::start_note(unsigned note)
|
|||||||
rEGR = GTIM_EGR_UG; // force a reload of the period
|
rEGR = GTIM_EGR_UG; // force a reload of the period
|
||||||
rCCER |= TONE_CCER; // enable the output
|
rCCER |= TONE_CCER; // enable the output
|
||||||
|
|
||||||
|
// configure the GPIO to enable timer output
|
||||||
|
stm32_configgpio(GPIO_TONE_ALARM);
|
||||||
}
|
}
|
||||||
|
|
||||||
void
|
void
|
||||||
@@ -616,10 +618,8 @@ ToneAlarm::stop_note()
|
|||||||
|
|
||||||
/*
|
/*
|
||||||
* Make sure the GPIO is not driving the speaker.
|
* Make sure the GPIO is not driving the speaker.
|
||||||
*
|
|
||||||
* XXX this presumes PX4FMU and the onboard speaker driver FET.
|
|
||||||
*/
|
*/
|
||||||
stm32_gpiowrite(GPIO_TONE_ALARM, 0);
|
stm32_configgpio(GPIO_TONE_ALARM_IDLE);
|
||||||
}
|
}
|
||||||
|
|
||||||
void
|
void
|
||||||
|
|||||||
@@ -355,6 +355,8 @@ int KalmanNav::predictState(float dt)
|
|||||||
float LDot = vN / R;
|
float LDot = vN / R;
|
||||||
float lDot = vE / (cosLSing * R);
|
float lDot = vE / (cosLSing * R);
|
||||||
float rotRate = 2 * omega + lDot;
|
float rotRate = 2 * omega + lDot;
|
||||||
|
|
||||||
|
// XXX position prediction using speed
|
||||||
float vNDot = fN - vE * rotRate * sinL +
|
float vNDot = fN - vE * rotRate * sinL +
|
||||||
vD * LDot;
|
vD * LDot;
|
||||||
float vDDot = fD - vE * rotRate * cosL -
|
float vDDot = fD - vE * rotRate * cosL -
|
||||||
|
|||||||
@@ -1,6 +1,6 @@
|
|||||||
############################################################################
|
############################################################################
|
||||||
#
|
#
|
||||||
# Copyright (C) 2012 PX4 Development Team. All rights reserved.
|
# Copyright (c) 2012, 2013 PX4 Development Team. All rights reserved.
|
||||||
#
|
#
|
||||||
# Redistribution and use in source and binary forms, with or without
|
# Redistribution and use in source and binary forms, with or without
|
||||||
# modification, are permitted provided that the following conditions
|
# modification, are permitted provided that the following conditions
|
||||||
@@ -32,7 +32,7 @@
|
|||||||
############################################################################
|
############################################################################
|
||||||
|
|
||||||
#
|
#
|
||||||
# Basic example application
|
# Full attitude / position Extended Kalman Filter
|
||||||
#
|
#
|
||||||
|
|
||||||
APPNAME = kalman_demo
|
APPNAME = kalman_demo
|
||||||
|
|||||||
@@ -64,6 +64,8 @@ ROOTDEPPATH = --dep-path .
|
|||||||
|
|
||||||
VPATH =
|
VPATH =
|
||||||
|
|
||||||
|
MAXOPTIMIZATION = -Os
|
||||||
|
|
||||||
all: .built
|
all: .built
|
||||||
.PHONY: clean depend distclean
|
.PHONY: clean depend distclean
|
||||||
|
|
||||||
|
|||||||
@@ -477,25 +477,27 @@ handle_message(mavlink_message_t *msg)
|
|||||||
|
|
||||||
/* gps */
|
/* gps */
|
||||||
hil_gps.timestamp_position = gps.time_usec;
|
hil_gps.timestamp_position = gps.time_usec;
|
||||||
// hil_gps.counter = hil_counter++;
|
|
||||||
hil_gps.time_gps_usec = gps.time_usec;
|
hil_gps.time_gps_usec = gps.time_usec;
|
||||||
hil_gps.lat = gps.lat;
|
hil_gps.lat = gps.lat;
|
||||||
hil_gps.lon = gps.lon;
|
hil_gps.lon = gps.lon;
|
||||||
hil_gps.alt = gps.alt;
|
hil_gps.alt = gps.alt;
|
||||||
// hil_gps.counter_pos_valid = hil_counter++;
|
|
||||||
hil_gps.eph_m = (float)gps.eph * 1e-2f; // from cm to m
|
hil_gps.eph_m = (float)gps.eph * 1e-2f; // from cm to m
|
||||||
hil_gps.epv_m = (float)gps.epv * 1e-2f; // from cm to m
|
hil_gps.epv_m = (float)gps.epv * 1e-2f; // from cm to m
|
||||||
hil_gps.s_variance_m_s = 5.0f;
|
hil_gps.s_variance_m_s = 5.0f;
|
||||||
hil_gps.p_variance_m = hil_gps.eph_m * hil_gps.eph_m;
|
hil_gps.p_variance_m = hil_gps.eph_m * hil_gps.eph_m;
|
||||||
hil_gps.vel_m_s = (float)gps.vel * 1e-2f; // from cm/s to m/s
|
hil_gps.vel_m_s = (float)gps.vel * 1e-2f; // from cm/s to m/s
|
||||||
|
|
||||||
/* gps.cog is in degrees 0..360 * 100, heading is -PI..PI */
|
/* gps.cog is in degrees 0..360 * 100, heading is -PI..+PI */
|
||||||
float heading_rad = gps.cog * M_DEG_TO_RAD_F * 1e-2f - M_PI_F;
|
float heading_rad = gps.cog * M_DEG_TO_RAD_F * 1e-2f;
|
||||||
|
/* go back to -PI..PI */
|
||||||
|
if (heading_rad > M_PI_F)
|
||||||
|
heading_rad -= 2.0f * M_PI_F;
|
||||||
hil_gps.vel_n_m_s = (float)gps.vel * 1e-2f * cosf(heading_rad);
|
hil_gps.vel_n_m_s = (float)gps.vel * 1e-2f * cosf(heading_rad);
|
||||||
hil_gps.vel_e_m_s = (float)gps.vel * 1e-2f * sinf(heading_rad);
|
hil_gps.vel_e_m_s = (float)gps.vel * 1e-2f * sinf(heading_rad);
|
||||||
hil_gps.vel_d_m_s = 0.0f;
|
hil_gps.vel_d_m_s = 0.0f;
|
||||||
/* COG (course over ground) is speced as 0..360 degrees (compass) */
|
hil_gps.vel_ned_valid = true;
|
||||||
hil_gps.cog_rad = heading_rad + M_PI_F; // from deg*100 to rad
|
/* COG (course over ground) is speced as -PI..+PI */
|
||||||
|
hil_gps.cog_rad = heading_rad;
|
||||||
hil_gps.fix_type = gps.fix_type;
|
hil_gps.fix_type = gps.fix_type;
|
||||||
hil_gps.satellites_visible = gps.satellites_visible;
|
hil_gps.satellites_visible = gps.satellites_visible;
|
||||||
|
|
||||||
|
|||||||
@@ -229,6 +229,13 @@ l_vehicle_gps_position(const struct listener *l)
|
|||||||
/* copy gps data into local buffer */
|
/* copy gps data into local buffer */
|
||||||
orb_copy(ORB_ID(vehicle_gps_position), mavlink_subs.gps_sub, &gps);
|
orb_copy(ORB_ID(vehicle_gps_position), mavlink_subs.gps_sub, &gps);
|
||||||
|
|
||||||
|
/* GPS COG is 0..2PI in degrees * 1e2 */
|
||||||
|
float cog_deg = gps.cog_rad;
|
||||||
|
if (cog_deg > M_PI_F)
|
||||||
|
cog_deg -= 2.0f * M_PI_F;
|
||||||
|
cog_deg *= M_RAD_TO_DEG_F;
|
||||||
|
|
||||||
|
|
||||||
/* GPS position */
|
/* GPS position */
|
||||||
mavlink_msg_gps_raw_int_send(MAVLINK_COMM_0,
|
mavlink_msg_gps_raw_int_send(MAVLINK_COMM_0,
|
||||||
gps.timestamp_position,
|
gps.timestamp_position,
|
||||||
@@ -236,13 +243,14 @@ l_vehicle_gps_position(const struct listener *l)
|
|||||||
gps.lat,
|
gps.lat,
|
||||||
gps.lon,
|
gps.lon,
|
||||||
gps.alt,
|
gps.alt,
|
||||||
(uint16_t)(gps.eph_m * 1e2f), // from m to cm
|
gps.eph_m * 1e2f, // from m to cm
|
||||||
(uint16_t)(gps.epv_m * 1e2f), // from m to cm
|
gps.epv_m * 1e2f, // from m to cm
|
||||||
(uint16_t)(gps.vel_m_s * 1e2f), // from m/s to cm/s
|
gps.vel_m_s * 1e2f, // from m/s to cm/s
|
||||||
(uint16_t)(gps.cog_rad * M_RAD_TO_DEG_F * 1e2f), // from rad to deg * 100
|
cog_deg * 1e2f, // from rad to deg * 100
|
||||||
gps.satellites_visible);
|
gps.satellites_visible);
|
||||||
|
|
||||||
if (gps.satellite_info_available && (gps_counter % 4 == 0)) {
|
/* update SAT info every 10 seconds */
|
||||||
|
if (gps.satellite_info_available && (gps_counter % 50 == 0)) {
|
||||||
mavlink_msg_gps_status_send(MAVLINK_COMM_0,
|
mavlink_msg_gps_status_send(MAVLINK_COMM_0,
|
||||||
gps.satellites_visible,
|
gps.satellites_visible,
|
||||||
gps.satellite_prn,
|
gps.satellite_prn,
|
||||||
|
|||||||
@@ -107,6 +107,8 @@ endif
|
|||||||
ROOTDEPPATH = --dep-path .
|
ROOTDEPPATH = --dep-path .
|
||||||
VPATH =
|
VPATH =
|
||||||
|
|
||||||
|
MAXOPTIMIZATION = -Os
|
||||||
|
|
||||||
# Build targets
|
# Build targets
|
||||||
|
|
||||||
all: .built
|
all: .built
|
||||||
|
|||||||
@@ -40,3 +40,5 @@ PRIORITY = SCHED_PRIORITY_DEFAULT
|
|||||||
STACKSIZE = 12000
|
STACKSIZE = 12000
|
||||||
|
|
||||||
include $(APPDIR)/mk/app.mk
|
include $(APPDIR)/mk/app.mk
|
||||||
|
|
||||||
|
MAXOPTIMIZATION = -Os
|
||||||
|
|||||||
@@ -64,6 +64,7 @@ VPATH =
|
|||||||
APPNAME = i2c
|
APPNAME = i2c
|
||||||
PRIORITY = SCHED_PRIORITY_DEFAULT
|
PRIORITY = SCHED_PRIORITY_DEFAULT
|
||||||
STACKSIZE = 2048
|
STACKSIZE = 2048
|
||||||
|
MAXOPTIMIZATION = -Os
|
||||||
|
|
||||||
# Build targets
|
# Build targets
|
||||||
|
|
||||||
|
|||||||
@@ -40,3 +40,5 @@ PRIORITY = SCHED_PRIORITY_DEFAULT
|
|||||||
STACKSIZE = 4096
|
STACKSIZE = 4096
|
||||||
|
|
||||||
include $(APPDIR)/mk/app.mk
|
include $(APPDIR)/mk/app.mk
|
||||||
|
|
||||||
|
MAXOPTIMIZATION = -Os
|
||||||
|
|||||||
@@ -40,3 +40,5 @@ PRIORITY = SCHED_PRIORITY_DEFAULT
|
|||||||
STACKSIZE = 2048
|
STACKSIZE = 2048
|
||||||
|
|
||||||
include $(APPDIR)/mk/app.mk
|
include $(APPDIR)/mk/app.mk
|
||||||
|
|
||||||
|
MAXOPTIMIZATION = -Os
|
||||||
|
|||||||
@@ -40,3 +40,5 @@ PRIORITY = SCHED_PRIORITY_MAX - 1
|
|||||||
STACKSIZE = 4096
|
STACKSIZE = 4096
|
||||||
|
|
||||||
include $(APPDIR)/mk/app.mk
|
include $(APPDIR)/mk/app.mk
|
||||||
|
|
||||||
|
MAXOPTIMIZATION = -Os
|
||||||
|
|||||||
@@ -40,3 +40,5 @@ PRIORITY = SCHED_PRIORITY_DEFAULT
|
|||||||
STACKSIZE = 2048
|
STACKSIZE = 2048
|
||||||
|
|
||||||
include $(APPDIR)/mk/app.mk
|
include $(APPDIR)/mk/app.mk
|
||||||
|
|
||||||
|
MAXOPTIMIZATION = -Os
|
||||||
|
|||||||
@@ -40,3 +40,5 @@ PRIORITY = SCHED_PRIORITY_DEFAULT
|
|||||||
STACKSIZE = 4096
|
STACKSIZE = 4096
|
||||||
|
|
||||||
include $(APPDIR)/mk/app.mk
|
include $(APPDIR)/mk/app.mk
|
||||||
|
|
||||||
|
MAXOPTIMIZATION = -Os
|
||||||
|
|||||||
@@ -40,3 +40,5 @@ PRIORITY = SCHED_PRIORITY_DEFAULT
|
|||||||
STACKSIZE = 4096
|
STACKSIZE = 4096
|
||||||
|
|
||||||
include $(APPDIR)/mk/app.mk
|
include $(APPDIR)/mk/app.mk
|
||||||
|
|
||||||
|
MAXOPTIMIZATION = -Os
|
||||||
|
|||||||
@@ -40,3 +40,5 @@ PRIORITY = SCHED_PRIORITY_DEFAULT
|
|||||||
STACKSIZE = 4096
|
STACKSIZE = 4096
|
||||||
|
|
||||||
include $(APPDIR)/mk/app.mk
|
include $(APPDIR)/mk/app.mk
|
||||||
|
|
||||||
|
MAXOPTIMIZATION = -Os
|
||||||
|
|||||||
@@ -40,3 +40,5 @@ PRIORITY = SCHED_PRIORITY_DEFAULT
|
|||||||
STACKSIZE = 2048
|
STACKSIZE = 2048
|
||||||
|
|
||||||
include $(APPDIR)/mk/app.mk
|
include $(APPDIR)/mk/app.mk
|
||||||
|
|
||||||
|
MAXOPTIMIZATION = -Os
|
||||||
|
|||||||
@@ -40,3 +40,5 @@ PRIORITY = SCHED_PRIORITY_DEFAULT
|
|||||||
STACKSIZE = 2048
|
STACKSIZE = 2048
|
||||||
|
|
||||||
include $(APPDIR)/mk/app.mk
|
include $(APPDIR)/mk/app.mk
|
||||||
|
|
||||||
|
MAXOPTIMIZATION = -Os
|
||||||
|
|||||||
@@ -40,3 +40,5 @@ PRIORITY = SCHED_PRIORITY_DEFAULT
|
|||||||
STACKSIZE = 2048
|
STACKSIZE = 2048
|
||||||
|
|
||||||
include $(APPDIR)/mk/app.mk
|
include $(APPDIR)/mk/app.mk
|
||||||
|
|
||||||
|
MAXOPTIMIZATION = -Os
|
||||||
|
|||||||
@@ -40,3 +40,5 @@ PRIORITY = SCHED_PRIORITY_DEFAULT - 10
|
|||||||
STACKSIZE = 3000
|
STACKSIZE = 3000
|
||||||
|
|
||||||
include $(APPDIR)/mk/app.mk
|
include $(APPDIR)/mk/app.mk
|
||||||
|
|
||||||
|
MAXOPTIMIZATION = -Os
|
||||||
|
|||||||
@@ -418,6 +418,7 @@ public:
|
|||||||
enum Geometry {
|
enum Geometry {
|
||||||
QUAD_X = 0, /**< quad in X configuration */
|
QUAD_X = 0, /**< quad in X configuration */
|
||||||
QUAD_PLUS, /**< quad in + configuration */
|
QUAD_PLUS, /**< quad in + configuration */
|
||||||
|
QUAD_V, /**< quad in V configuration */
|
||||||
HEX_X, /**< hex in X configuration */
|
HEX_X, /**< hex in X configuration */
|
||||||
HEX_PLUS, /**< hex in + configuration */
|
HEX_PLUS, /**< hex in + configuration */
|
||||||
OCTA_X,
|
OCTA_X,
|
||||||
|
|||||||
@@ -82,6 +82,12 @@ const MultirotorMixer::Rotor _config_quad_plus[] = {
|
|||||||
{ 0.000000, 1.000000, -1.00 },
|
{ 0.000000, 1.000000, -1.00 },
|
||||||
{ -0.000000, -1.000000, -1.00 },
|
{ -0.000000, -1.000000, -1.00 },
|
||||||
};
|
};
|
||||||
|
const MultirotorMixer::Rotor _config_quad_v[] = {
|
||||||
|
{ -0.927184, 0.374607, 1.00 },
|
||||||
|
{ 0.694658, -0.719340, 1.00 },
|
||||||
|
{ 0.927184, 0.374607, -1.00 },
|
||||||
|
{ -0.694658, -0.719340, -1.00 },
|
||||||
|
};
|
||||||
const MultirotorMixer::Rotor _config_hex_x[] = {
|
const MultirotorMixer::Rotor _config_hex_x[] = {
|
||||||
{ -1.000000, 0.000000, -1.00 },
|
{ -1.000000, 0.000000, -1.00 },
|
||||||
{ 1.000000, 0.000000, 1.00 },
|
{ 1.000000, 0.000000, 1.00 },
|
||||||
@@ -121,6 +127,7 @@ const MultirotorMixer::Rotor _config_octa_plus[] = {
|
|||||||
const MultirotorMixer::Rotor *_config_index[MultirotorMixer::Geometry::MAX_GEOMETRY] = {
|
const MultirotorMixer::Rotor *_config_index[MultirotorMixer::Geometry::MAX_GEOMETRY] = {
|
||||||
&_config_quad_x[0],
|
&_config_quad_x[0],
|
||||||
&_config_quad_plus[0],
|
&_config_quad_plus[0],
|
||||||
|
&_config_quad_v[0],
|
||||||
&_config_hex_x[0],
|
&_config_hex_x[0],
|
||||||
&_config_hex_plus[0],
|
&_config_hex_plus[0],
|
||||||
&_config_octa_x[0],
|
&_config_octa_x[0],
|
||||||
@@ -129,6 +136,7 @@ const MultirotorMixer::Rotor *_config_index[MultirotorMixer::Geometry::MAX_GEOME
|
|||||||
const unsigned _config_rotor_count[MultirotorMixer::Geometry::MAX_GEOMETRY] = {
|
const unsigned _config_rotor_count[MultirotorMixer::Geometry::MAX_GEOMETRY] = {
|
||||||
4, /* quad_x */
|
4, /* quad_x */
|
||||||
4, /* quad_plus */
|
4, /* quad_plus */
|
||||||
|
4, /* quad_v */
|
||||||
6, /* hex_x */
|
6, /* hex_x */
|
||||||
6, /* hex_plus */
|
6, /* hex_plus */
|
||||||
8, /* octa_x */
|
8, /* octa_x */
|
||||||
@@ -184,6 +192,9 @@ MultirotorMixer::from_text(Mixer::ControlCallback control_cb, uintptr_t cb_handl
|
|||||||
} else if (!strcmp(geomname, "4x")) {
|
} else if (!strcmp(geomname, "4x")) {
|
||||||
geometry = MultirotorMixer::QUAD_X;
|
geometry = MultirotorMixer::QUAD_X;
|
||||||
|
|
||||||
|
} else if (!strcmp(geomname, "4v")) {
|
||||||
|
geometry = MultirotorMixer::QUAD_V;
|
||||||
|
|
||||||
} else if (!strcmp(geomname, "6+")) {
|
} else if (!strcmp(geomname, "6+")) {
|
||||||
geometry = MultirotorMixer::HEX_PLUS;
|
geometry = MultirotorMixer::HEX_PLUS;
|
||||||
|
|
||||||
|
|||||||
@@ -20,6 +20,13 @@ set quad_plus {
|
|||||||
180 CW
|
180 CW
|
||||||
}
|
}
|
||||||
|
|
||||||
|
set quad_v {
|
||||||
|
68 CCW
|
||||||
|
-136 CCW
|
||||||
|
-68 CW
|
||||||
|
136 CW
|
||||||
|
}
|
||||||
|
|
||||||
set hex_x {
|
set hex_x {
|
||||||
90 CW
|
90 CW
|
||||||
-90 CCW
|
-90 CCW
|
||||||
@@ -60,7 +67,7 @@ set octa_plus {
|
|||||||
90 CW
|
90 CW
|
||||||
}
|
}
|
||||||
|
|
||||||
set tables {quad_x quad_plus hex_x hex_plus octa_x octa_plus}
|
set tables {quad_x quad_plus quad_v hex_x hex_plus octa_x octa_plus}
|
||||||
|
|
||||||
proc factors {a d} { puts [format "\t{ %9.6f, %9.6f, %5.2f }," [rcos [expr $a + 90]] [rcos $a] [expr -$d]]}
|
proc factors {a d} { puts [format "\t{ %9.6f, %9.6f, %5.2f }," [rcos [expr $a + 90]] [rcos $a] [expr -$d]]}
|
||||||
|
|
||||||
|
|||||||
@@ -55,38 +55,39 @@
|
|||||||
*/
|
*/
|
||||||
struct vehicle_gps_position_s
|
struct vehicle_gps_position_s
|
||||||
{
|
{
|
||||||
uint64_t timestamp_position; /**< Timestamp for position information */
|
uint64_t timestamp_position; /**< Timestamp for position information */
|
||||||
int32_t lat; /**< Latitude in 1E7 degrees */
|
int32_t lat; /**< Latitude in 1E7 degrees */
|
||||||
int32_t lon; /**< Longitude in 1E7 degrees */
|
int32_t lon; /**< Longitude in 1E7 degrees */
|
||||||
int32_t alt; /**< Altitude in 1E3 meters (millimeters) above MSL */
|
int32_t alt; /**< Altitude in 1E3 meters (millimeters) above MSL */
|
||||||
|
|
||||||
uint64_t timestamp_variance;
|
uint64_t timestamp_variance;
|
||||||
float s_variance_m_s; /**< speed accuracy estimate m/s */
|
float s_variance_m_s; /**< speed accuracy estimate m/s */
|
||||||
float p_variance_m; /**< position accuracy estimate m */
|
float p_variance_m; /**< position accuracy estimate m */
|
||||||
uint8_t fix_type; /**< 0-1: no fix, 2: 2D fix, 3: 3D fix. Some applications will not use the value of this field unless it is at least two, so always correctly fill in the fix. */
|
float c_variance_rad; /**< course accuracy estimate rad */
|
||||||
|
uint8_t fix_type; /**< 0-1: no fix, 2: 2D fix, 3: 3D fix. Some applications will not use the value of this field unless it is at least two, so always correctly fill in the fix. */
|
||||||
|
|
||||||
float eph_m; /**< GPS HDOP horizontal dilution of position in m */
|
float eph_m; /**< GPS HDOP horizontal dilution of position in m */
|
||||||
float epv_m; /**< GPS VDOP horizontal dilution of position in m */
|
float epv_m; /**< GPS VDOP horizontal dilution of position in m */
|
||||||
|
|
||||||
uint64_t timestamp_velocity; /**< Timestamp for velocity informations */
|
uint64_t timestamp_velocity; /**< Timestamp for velocity informations */
|
||||||
float vel_m_s; /**< GPS ground speed (m/s) */
|
float vel_m_s; /**< GPS ground speed (m/s) */
|
||||||
float vel_n_m_s; /**< GPS ground speed in m/s */
|
float vel_n_m_s; /**< GPS ground speed in m/s */
|
||||||
float vel_e_m_s; /**< GPS ground speed in m/s */
|
float vel_e_m_s; /**< GPS ground speed in m/s */
|
||||||
float vel_d_m_s; /**< GPS ground speed in m/s */
|
float vel_d_m_s; /**< GPS ground speed in m/s */
|
||||||
float cog_rad; /**< Course over ground (NOT heading, but direction of movement) in rad */
|
float cog_rad; /**< Course over ground (NOT heading, but direction of movement) in rad, -PI..PI */
|
||||||
bool vel_ned_valid; /**< Flag to indicate if NED speed is valid */
|
bool vel_ned_valid; /**< Flag to indicate if NED speed is valid */
|
||||||
|
|
||||||
uint64_t timestamp_time; /**< Timestamp for time information */
|
uint64_t timestamp_time; /**< Timestamp for time information */
|
||||||
uint64_t time_gps_usec; /**< Timestamp (microseconds in GPS format), this is the timestamp which comes from the gps module */
|
uint64_t time_gps_usec; /**< Timestamp (microseconds in GPS format), this is the timestamp which comes from the gps module */
|
||||||
|
|
||||||
uint64_t timestamp_satellites; /**< Timestamp for sattelite information */
|
uint64_t timestamp_satellites; /**< Timestamp for sattelite information */
|
||||||
uint8_t satellites_visible; /**< Number of satellites visible. If unknown, set to 255 */
|
uint8_t satellites_visible; /**< Number of satellites visible. If unknown, set to 255 */
|
||||||
uint8_t satellite_prn[20]; /**< Global satellite ID */
|
uint8_t satellite_prn[20]; /**< Global satellite ID */
|
||||||
uint8_t satellite_used[20]; /**< 0: Satellite not used, 1: used for localization */
|
uint8_t satellite_used[20]; /**< 0: Satellite not used, 1: used for localization */
|
||||||
uint8_t satellite_elevation[20]; /**< Elevation (0: right on top of receiver, 90: on the horizon) of satellite */
|
uint8_t satellite_elevation[20]; /**< Elevation (0: right on top of receiver, 90: on the horizon) of satellite */
|
||||||
uint8_t satellite_azimuth[20]; /**< Direction of satellite, 0: 0 deg, 255: 360 deg. */
|
uint8_t satellite_azimuth[20]; /**< Direction of satellite, 0: 0 deg, 255: 360 deg. */
|
||||||
uint8_t satellite_snr[20]; /**< Signal to noise ratio of satellite */
|
uint8_t satellite_snr[20]; /**< Signal to noise ratio of satellite */
|
||||||
bool satellite_info_available; /**< 0 for no info, 1 for info available */
|
bool satellite_info_available; /**< 0 for no info, 1 for info available */
|
||||||
};
|
};
|
||||||
|
|
||||||
/**
|
/**
|
||||||
|
|||||||
@@ -326,6 +326,7 @@
|
|||||||
*/
|
*/
|
||||||
#define TONE_ALARM_TIMER 3 /* timer 3 */
|
#define TONE_ALARM_TIMER 3 /* timer 3 */
|
||||||
#define TONE_ALARM_CHANNEL 3 /* channel 3 */
|
#define TONE_ALARM_CHANNEL 3 /* channel 3 */
|
||||||
|
#define GPIO_TONE_ALARM_IDLE (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTC|GPIO_PIN8)
|
||||||
#define GPIO_TONE_ALARM (GPIO_ALT|GPIO_AF2|GPIO_SPEED_2MHz|GPIO_FLOAT|GPIO_PUSHPULL|GPIO_PORTC|GPIO_PIN8)
|
#define GPIO_TONE_ALARM (GPIO_ALT|GPIO_AF2|GPIO_SPEED_2MHz|GPIO_FLOAT|GPIO_PUSHPULL|GPIO_PORTC|GPIO_PIN8)
|
||||||
|
|
||||||
/************************************************************************************
|
/************************************************************************************
|
||||||
|
|||||||
@@ -124,6 +124,7 @@ CONFIGURED_APPS += drivers/blinkm
|
|||||||
CONFIGURED_APPS += drivers/stm32/tone_alarm
|
CONFIGURED_APPS += drivers/stm32/tone_alarm
|
||||||
CONFIGURED_APPS += drivers/stm32/adc
|
CONFIGURED_APPS += drivers/stm32/adc
|
||||||
CONFIGURED_APPS += drivers/px4fmu
|
CONFIGURED_APPS += drivers/px4fmu
|
||||||
|
CONFIGURED_APPS += drivers/mkblctrl
|
||||||
CONFIGURED_APPS += drivers/hil
|
CONFIGURED_APPS += drivers/hil
|
||||||
CONFIGURED_APPS += drivers/gps
|
CONFIGURED_APPS += drivers/gps
|
||||||
CONFIGURED_APPS += drivers/mb12xx
|
CONFIGURED_APPS += drivers/mb12xx
|
||||||
|
|||||||
@@ -112,7 +112,6 @@ ARCHOPTIMIZATION = $(MAXOPTIMIZATION) \
|
|||||||
|
|
||||||
ifeq ("${CONFIG_DEBUG_SYMBOLS}","y")
|
ifeq ("${CONFIG_DEBUG_SYMBOLS}","y")
|
||||||
ARCHOPTIMIZATION += -g
|
ARCHOPTIMIZATION += -g
|
||||||
ARCHSCRIPT += -g
|
|
||||||
endif
|
endif
|
||||||
|
|
||||||
ARCHCFLAGS = -std=gnu99
|
ARCHCFLAGS = -std=gnu99
|
||||||
@@ -145,7 +144,7 @@ ARCHDEFINES =
|
|||||||
ARCHPICFLAGS = -fpic -msingle-pic-base -mpic-register=r10
|
ARCHPICFLAGS = -fpic -msingle-pic-base -mpic-register=r10
|
||||||
|
|
||||||
# this seems to be the only way to add linker flags
|
# this seems to be the only way to add linker flags
|
||||||
ARCHSCRIPT += --warn-common \
|
EXTRA_LIBS += --warn-common \
|
||||||
--gc-sections
|
--gc-sections
|
||||||
|
|
||||||
CFLAGS = $(ARCHCFLAGS) $(ARCHCWARNINGS) $(ARCHOPTIMIZATION) $(ARCHCPUFLAGS) $(ARCHINCLUDES) $(INSTRUMENTATIONDEFINES) $(ARCHDEFINES) $(EXTRADEFINES) -pipe -fno-common
|
CFLAGS = $(ARCHCFLAGS) $(ARCHCWARNINGS) $(ARCHOPTIMIZATION) $(ARCHCPUFLAGS) $(ARCHINCLUDES) $(INSTRUMENTATIONDEFINES) $(ARCHDEFINES) $(EXTRADEFINES) -pipe -fno-common
|
||||||
|
|||||||
Reference in New Issue
Block a user