Merged master

This commit is contained in:
Lorenz Meier
2014-07-12 16:11:43 +02:00
18 changed files with 249 additions and 110 deletions
+33 -35
View File
@@ -133,26 +133,44 @@ SPI::probe()
int
SPI::transfer(uint8_t *send, uint8_t *recv, unsigned len)
{
irqstate_t state;
int result;
if ((send == nullptr) && (recv == nullptr))
return -EINVAL;
/* lock the bus as required */
if (!up_interrupt_context()) {
switch (locking_mode) {
default:
case LOCK_PREEMPTION:
state = irqsave();
break;
case LOCK_THREADS:
SPI_LOCK(_dev, true);
break;
case LOCK_NONE:
break;
}
}
LockMode mode = up_interrupt_context() ? LOCK_NONE : locking_mode;
/* lock the bus as required */
switch (mode) {
default:
case LOCK_PREEMPTION:
{
irqstate_t state = irqsave();
result = _transfer(send, recv, len);
irqrestore(state);
}
break;
case LOCK_THREADS:
SPI_LOCK(_dev, true);
result = _transfer(send, recv, len);
SPI_LOCK(_dev, false);
break;
case LOCK_NONE:
result = _transfer(send, recv, len);
break;
}
return result;
}
void
SPI::set_frequency(uint32_t frequency)
{
_frequency = frequency;
}
int
SPI::_transfer(uint8_t *send, uint8_t *recv, unsigned len)
{
SPI_SETFREQUENCY(_dev, _frequency);
SPI_SETMODE(_dev, _mode);
SPI_SETBITS(_dev, 8);
@@ -164,27 +182,7 @@ SPI::transfer(uint8_t *send, uint8_t *recv, unsigned len)
/* and clean up */
SPI_SELECT(_dev, _device, false);
if (!up_interrupt_context()) {
switch (locking_mode) {
default:
case LOCK_PREEMPTION:
irqrestore(state);
break;
case LOCK_THREADS:
SPI_LOCK(_dev, false);
break;
case LOCK_NONE:
break;
}
}
return OK;
}
void
SPI::set_frequency(uint32_t frequency)
{
_frequency = frequency;
}
} // namespace device
+2
View File
@@ -131,6 +131,8 @@ private:
protected:
int _bus;
int _transfer(uint8_t *send, uint8_t *recv, unsigned len);
};
} // namespace device
+14 -2
View File
@@ -46,10 +46,18 @@
#define PX4FLOW_DEVICE_PATH "/dev/px4flow"
/**
* @addtogroup topics
* @{
*/
/**
* Optical flow in NED body frame in SI units.
*
* @see http://en.wikipedia.org/wiki/International_System_of_Units
*
* @warning If possible the usage of the raw flow and performing rotation-compensation
* using the autopilot angular rate estimate is recommended.
*/
struct px4flow_report {
@@ -57,14 +65,18 @@ struct px4flow_report {
int16_t flow_raw_x; /**< flow in pixels in X direction, not rotation-compensated */
int16_t flow_raw_y; /**< flow in pixels in Y direction, not rotation-compensated */
float flow_comp_x_m; /**< speed over ground in meters, rotation-compensated */
float flow_comp_y_m; /**< speed over ground in meters, rotation-compensated */
float flow_comp_x_m; /**< speed over ground in meters per second, rotation-compensated */
float flow_comp_y_m; /**< speed over ground in meters per second, rotation-compensated */
float ground_distance_m; /**< Altitude / distance to ground in meters */
uint8_t quality; /**< Quality of the measurement, 0: bad quality, 255: maximum quality */
uint8_t sensor_id; /**< id of the sensor emitting the flow value */
};
/**
* @}
*/
/*
* ObjDev tag for px4flow data.
*/
+9
View File
@@ -50,6 +50,11 @@ enum RANGE_FINDER_TYPE {
RANGE_FINDER_TYPE_LASER = 0,
};
/**
* @addtogroup topics
* @{
*/
/**
* range finder report structure. Reads from the device must be in multiples of this
* structure.
@@ -64,6 +69,10 @@ struct range_finder_report {
uint8_t valid; /**< 1 == within sensor range, 0 = outside sensor range */
};
/**
* @}
*/
/*
* ObjDev tag for raw range finder data.
*/
+9
View File
@@ -67,6 +67,11 @@
*/
#define RC_INPUT_RSSI_MAX 255
/**
* @addtogroup topics
* @{
*/
/**
* Input signal type, value is a control position from zero to 100
* percent.
@@ -141,6 +146,10 @@ struct rc_input_values {
rc_input_t values[RC_INPUT_MAX_CHANNELS];
};
/**
* @}
*/
/*
* ObjDev tag for R/C inputs.
*/
+3 -1
View File
@@ -127,7 +127,7 @@ private:
/**
* Try to configure the GPS, handle outgoing communication to the GPS
*/
void config();
void config();
/**
* Trampoline to the worker task
@@ -486,6 +486,8 @@ GPS::print_info()
warnx("position lock: %dD, satellites: %d, last update: %8.4fms ago", (int)_report_gps_pos.fix_type,
_report_gps_pos.satellites_used, (double)(hrt_absolute_time() - _report_gps_pos.timestamp_position) / 1000.0);
warnx("lat: %d, lon: %d, alt: %d", _report_gps_pos.lat, _report_gps_pos.lon, _report_gps_pos.alt);
warnx("vel: %.2fm/s, %.2fm/s, %.2fm/s", (double)_report_gps_pos.vel_n_m_s,
(double)_report_gps_pos.vel_e_m_s, (double)_report_gps_pos.vel_d_m_s);
warnx("eph: %.2fm, epv: %.2fm", (double)_report_gps_pos.eph, (double)_report_gps_pos.epv);
warnx("rate position: \t%6.2f Hz", (double)_Helper->get_position_update_rate());
warnx("rate velocity: \t%6.2f Hz", (double)_Helper->get_velocity_update_rate());
+1 -1
View File
@@ -329,7 +329,7 @@ PX4FMU::init()
_task = task_spawn_cmd("fmuservo",
SCHED_DEFAULT,
SCHED_PRIORITY_DEFAULT,
2048,
1600,
(main_t)&PX4FMU::task_main_trampoline,
nullptr);
+17 -5
View File
@@ -39,6 +39,7 @@
#include <nuttx/config.h>
#include <sys/types.h>
#include <stdlib.h>
#include <stdint.h>
#include <stdbool.h>
#include <assert.h>
@@ -413,11 +414,17 @@ static int read_with_retry(int fd, void *buf, size_t n)
int
PX4IO_Uploader::program(size_t fw_size)
{
uint8_t file_buf[PROG_MULTI_MAX];
uint8_t *file_buf;
ssize_t count;
int ret;
size_t sent = 0;
file_buf = (uint8_t *)malloc(PROG_MULTI_MAX);
if (!file_buf) {
log("Can't allocate program buffer");
return -ENOMEM;
}
log("programming %u bytes...", (unsigned)fw_size);
ret = lseek(_fw_fd, 0, SEEK_SET);
@@ -425,8 +432,8 @@ PX4IO_Uploader::program(size_t fw_size)
while (sent < fw_size) {
/* get more bytes to program */
size_t n = fw_size - sent;
if (n > sizeof(file_buf)) {
n = sizeof(file_buf);
if (n > PROG_MULTI_MAX) {
n = PROG_MULTI_MAX;
}
count = read_with_retry(_fw_fd, file_buf, n);
@@ -438,8 +445,10 @@ PX4IO_Uploader::program(size_t fw_size)
(int)errno);
}
if (count == 0)
if (count == 0) {
free(file_buf);
return OK;
}
sent += count;
@@ -455,9 +464,12 @@ PX4IO_Uploader::program(size_t fw_size)
ret = get_sync(1000);
if (ret != OK)
if (ret != OK) {
free(file_buf);
return ret;
}
}
free(file_buf);
return OK;
}
+16 -8
View File
@@ -286,15 +286,22 @@ int commander_main(int argc, char *argv[])
exit(0);
}
/* commands needing the app to run below */
if (!thread_running) {
warnx("\tcommander not started");
exit(1);
}
if (!strcmp(argv[1], "status")) {
if (thread_running) {
warnx("\tcommander is running");
print_status();
} else {
warnx("\tcommander not started");
}
print_status();
exit(0);
}
if (!strcmp(argv[1], "check")) {
int mavlink_fd_local = open(MAVLINK_LOG_DEVICE, 0);
int checkres = prearm_check(&status, mavlink_fd_local);
close(mavlink_fd_local);
warnx("FINAL RESULT: %s", (checkres == 0) ? "OK" : "FAILED");
exit(0);
}
@@ -303,7 +310,7 @@ int commander_main(int argc, char *argv[])
exit(0);
}
if (!strcmp(argv[1], "2")) {
if (!strcmp(argv[1], "disarm")) {
arm_disarm(false, mavlink_fd, "command line");
exit(0);
}
@@ -324,6 +331,7 @@ void usage(const char *reason)
void print_status()
{
warnx("type: %s", (status.is_rotary_wing) ? "ROTARY" : "PLANE");
warnx("usb powered: %s", (on_usb_power) ? "yes" : "no");
/* read all relevant states */
+16 -19
View File
@@ -70,8 +70,6 @@
#endif
static const int ERROR = -1;
static int prearm_check(const struct vehicle_status_s *status, const int mavlink_fd);
// This array defines the arming state transitions. The rows are the new state, and the columns
// are the current state. Using new state and current state you can index into the array which
// will be true for a valid transition or false for a invalid transition. In some cases even
@@ -622,12 +620,13 @@ bool set_nav_state(struct vehicle_status_s *status, const bool data_link_loss_en
int prearm_check(const struct vehicle_status_s *status, const int mavlink_fd)
{
int ret;
bool failed = false;
int fd = open(ACCEL_DEVICE_PATH, O_RDONLY);
if (fd < 0) {
mavlink_log_critical(mavlink_fd, "#audio: FAIL: ACCEL SENSOR MISSING");
ret = fd;
failed = true;
goto system_eval;
}
@@ -635,6 +634,7 @@ int prearm_check(const struct vehicle_status_s *status, const int mavlink_fd)
if (ret != OK) {
mavlink_log_critical(mavlink_fd, "#audio: FAIL: ACCEL CALIBRATION");
failed = true;
goto system_eval;
}
@@ -644,33 +644,31 @@ int prearm_check(const struct vehicle_status_s *status, const int mavlink_fd)
if (ret == sizeof(acc)) {
/* evaluate values */
float accel_scale = sqrtf(acc.x * acc.x + acc.y * acc.y + acc.z * acc.z);
float accel_magnitude = sqrtf(acc.x * acc.x + acc.y * acc.y + acc.z * acc.z);
if (accel_scale < 9.78f || accel_scale > 9.83f) {
mavlink_log_info(mavlink_fd, "#audio: Accelerometer calibration recommended.");
}
if (accel_scale > 30.0f /* m/s^2 */) {
if (accel_magnitude < 4.0f || accel_magnitude > 15.0f /* m/s^2 */) {
mavlink_log_critical(mavlink_fd, "#audio: FAIL: ACCEL RANGE");
mavlink_log_info(mavlink_fd, "#audio: hold still while arming");
/* this is frickin' fatal */
ret = ERROR;
failed = true;
goto system_eval;
} else {
ret = OK;
}
} else {
mavlink_log_critical(mavlink_fd, "#audio: FAIL: ACCEL READ");
/* this is frickin' fatal */
ret = ERROR;
failed = true;
goto system_eval;
}
if (!status->is_rotary_wing) {
/* accel done, close it */
close(fd);
fd = open(AIRSPEED_DEVICE_PATH, O_RDONLY);
if (fd < 0) {
if (fd <= 0) {
mavlink_log_critical(mavlink_fd, "#audio: FAIL: AIRSPEED SENSOR MISSING");
ret = fd;
failed = true;
goto system_eval;
}
@@ -679,20 +677,19 @@ int prearm_check(const struct vehicle_status_s *status, const int mavlink_fd)
ret = read(fd, &diff_pres, sizeof(diff_pres));
if (ret == sizeof(diff_pres)) {
if (fabsf(diff_pres.differential_pressure_filtered_pa > 5.0f)) {
if (fabsf(diff_pres.differential_pressure_filtered_pa > 6.0f)) {
mavlink_log_critical(mavlink_fd, "#audio: WARNING AIRSPEED CALIBRATION MISSING");
// XXX do not make this fatal yet
ret = OK;
}
} else {
mavlink_log_critical(mavlink_fd, "#audio: FAIL: AIRSPEED READ");
/* this is frickin' fatal */
ret = ERROR;
failed = true;
goto system_eval;
}
}
system_eval:
close(fd);
return ret;
return (failed);
}
@@ -67,4 +67,6 @@ transition_result_t hil_state_transition(hil_state_t new_state, int status_pub,
bool set_nav_state(struct vehicle_status_s *status, const bool data_link_loss_enabled, const bool mission_finished);
int prearm_check(const struct vehicle_status_s *status, const int mavlink_fd);
#endif /* STATE_MACHINE_HELPER_H_ */
Submodule src/modules/ekf_att_pos_estimator/InertialNav added at 8b65d755b8
+23 -32
View File
@@ -1051,10 +1051,16 @@ protected:
uint32_t mavlink_custom_mode;
get_mavlink_mode_state(&status, &pos_sp_triplet, &mavlink_state, &mavlink_base_mode, &mavlink_custom_mode);
float out[8];
const float pwm_center = (PWM_HIGHEST_MAX + PWM_LOWEST_MIN) / 2;
/* scale outputs depending on system type */
if (mavlink_system.type == MAV_TYPE_QUADROTOR ||
mavlink_system.type == MAV_TYPE_HEXAROTOR ||
mavlink_system.type == MAV_TYPE_OCTOROTOR) {
/* set number of valid outputs depending on vehicle type */
/* multirotors: set number of rotor outputs depending on type */
unsigned n;
switch (mavlink_system.type) {
@@ -1071,59 +1077,44 @@ protected:
break;
}
/* scale / assign outputs depending on system type */
float out[8];
for (unsigned i = 0; i < 8; i++) {
if (i < n) {
if (mavlink_base_mode & MAV_MODE_FLAG_SAFETY_ARMED) {
/* scale fake PWM out 900..2100 us to 0..1 for normal multirotors */
if (mavlink_base_mode & MAV_MODE_FLAG_SAFETY_ARMED) {
if (i < n) {
/* scale PWM out 900..2100 us to 0..1 for rotors */
out[i] = (act.output[i] - PWM_LOWEST_MIN) / (PWM_HIGHEST_MAX - PWM_LOWEST_MIN);
} else {
/* send 0 when disarmed */
out[i] = 0.0f;
/* scale PWM out 900..2100 us to -1..1 for other channels */
out[i] = (act.output[i] - pwm_center) / ((PWM_HIGHEST_MAX - PWM_LOWEST_MIN) / 2);
}
} else {
out[i] = -1.0f;
/* send 0 when disarmed */
out[i] = 0.0f;
}
}
mavlink_msg_hil_controls_send(_channel,
hrt_absolute_time(),
out[0], out[1], out[2], out[3], out[4], out[5], out[6], out[7],
mavlink_base_mode,
0);
} else {
/* fixed wing: scale all channels except throttle -1 .. 1
* because we know that we set the mixers up this way
*/
float out[8];
const float pwm_center = (PWM_HIGHEST_MAX + PWM_LOWEST_MIN) / 2;
/* fixed wing: scale throttle to 0..1 and other channels to -1..1 */
for (unsigned i = 0; i < 8; i++) {
if (i != 3) {
/* scale fake PWM out 900..2100 us to -1..+1 for normal channels */
/* scale PWM out 900..2100 us to -1..1 for normal channels */
out[i] = (act.output[i] - pwm_center) / ((PWM_HIGHEST_MAX - PWM_LOWEST_MIN) / 2);
} else {
/* scale fake PWM out 900..2100 us to 0..1 for throttle */
/* scale PWM out 900..2100 us to 0..1 for throttle */
out[i] = (act.output[i] - PWM_LOWEST_MIN) / (PWM_HIGHEST_MAX - PWM_LOWEST_MIN);
}
}
mavlink_msg_hil_controls_send(_channel,
hrt_absolute_time(),
out[0], out[1], out[2], out[3], out[4], out[5], out[6], out[7],
mavlink_base_mode,
0);
}
mavlink_msg_hil_controls_send(_channel,
hrt_absolute_time(),
out[0], out[1], out[2], out[3], out[4], out[5], out[6], out[7],
mavlink_base_mode,
0);
}
}
};
+36 -1
View File
@@ -139,7 +139,14 @@ accel(int argc, char *argv[])
}
if (fabsf(buf.x) > 30.0f || fabsf(buf.y) > 30.0f || fabsf(buf.z) > 30.0f) {
warnx("ACCEL1 acceleration values out of range!");
warnx("ACCEL acceleration values out of range!");
return ERROR;
}
float len = sqrtf(buf.x * buf.x + buf.y * buf.y + buf.z * buf.z);
if (len < 8.0f || len > 12.0f) {
warnx("ACCEL scale error!");
return ERROR;
}
@@ -186,6 +193,13 @@ accel1(int argc, char *argv[])
return ERROR;
}
float len = sqrtf(buf.x * buf.x + buf.y * buf.y + buf.z * buf.z);
if (len < 8.0f || len > 12.0f) {
warnx("ACCEL1 scale error!");
return ERROR;
}
/* Let user know everything is ok */
printf("\tOK: ACCEL1 passed all tests successfully\n");
@@ -225,6 +239,13 @@ gyro(int argc, char *argv[])
printf("\tGYRO rates: x:%8.4f\ty:%8.4f\tz:%8.4f rad/s\n", (double)buf.x, (double)buf.y, (double)buf.z);
}
float len = sqrtf(buf.x * buf.x + buf.y * buf.y + buf.z * buf.z);
if (len > 0.3f) {
warnx("GYRO scale error!");
return ERROR;
}
/* Let user know everything is ok */
printf("\tOK: GYRO passed all tests successfully\n");
close(fd);
@@ -263,6 +284,13 @@ gyro1(int argc, char *argv[])
printf("\tGYRO1 rates: x:%8.4f\ty:%8.4f\tz:%8.4f rad/s\n", (double)buf.x, (double)buf.y, (double)buf.z);
}
float len = sqrtf(buf.x * buf.x + buf.y * buf.y + buf.z * buf.z);
if (len > 0.3f) {
warnx("GYRO1 scale error!");
return ERROR;
}
/* Let user know everything is ok */
printf("\tOK: GYRO1 passed all tests successfully\n");
close(fd);
@@ -301,6 +329,13 @@ mag(int argc, char *argv[])
printf("\tMAG values: x:%8.4f\ty:%8.4f\tz:%8.4f\n", (double)buf.x, (double)buf.y, (double)buf.z);
}
float len = sqrtf(buf.x * buf.x + buf.y * buf.y + buf.z * buf.z);
if (len < 1.0f || len > 3.0f) {
warnx("MAG scale error!");
return ERROR;
}
/* Let user know everything is ok */
printf("\tOK: MAG passed all tests successfully\n");
close(fd);