Merge branch 'master' into navigator_rewrite

Conflicts:
	src/drivers/gps/gps.cpp
	src/drivers/gps/mtk.cpp
	src/modules/commander/commander.cpp
	src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp
	src/modules/navigator/mission.cpp
	src/modules/navigator/mission.h
	src/modules/navigator/navigator_main.cpp
	src/modules/navigator/navigator_state.h
	src/modules/position_estimator_inav/position_estimator_inav_main.c
This commit is contained in:
Julian Oes
2014-05-26 20:19:11 +02:00
173 changed files with 5312 additions and 1890 deletions
+2 -1
View File
@@ -447,6 +447,7 @@ public:
QUAD_WIDE, /**< quad in wide configuration */
HEX_X, /**< hex in X configuration */
HEX_PLUS, /**< hex in + configuration */
HEX_COX,
OCTA_X,
OCTA_PLUS,
OCTA_COX,
@@ -516,7 +517,7 @@ private:
float _roll_scale;
float _pitch_scale;
float _yaw_scale;
float _deadband;
float _idle_speed;
unsigned _rotor_count;
const Rotor *_rotors;
@@ -67,6 +67,11 @@
namespace
{
float constrain(float val, float min, float max)
{
return (val < min) ? min : ((val > max) ? max : val);
}
/*
* These tables automatically generated by multi_tables - do not edit.
*/
@@ -110,6 +115,14 @@ const MultirotorMixer::Rotor _config_hex_plus[] = {
{ 0.866025, 0.500000, 1.00 },
{ -0.866025, -0.500000, -1.00 },
};
const MultirotorMixer::Rotor _config_hex_cox[] = {
{ -0.866025, 0.500000, -1.00 },
{ -0.866025, 0.500000, 1.00 },
{ -0.000000, -1.000000, -1.00 },
{ -0.000000, -1.000000, 1.00 },
{ 0.866025, 0.500000, -1.00 },
{ 0.866025, 0.500000, 1.00 },
};
const MultirotorMixer::Rotor _config_octa_x[] = {
{ -0.382683, 0.923880, -1.00 },
{ 0.382683, -0.923880, -1.00 },
@@ -147,6 +160,7 @@ const MultirotorMixer::Rotor *_config_index[MultirotorMixer::MAX_GEOMETRY] = {
&_config_quad_wide[0],
&_config_hex_x[0],
&_config_hex_plus[0],
&_config_hex_cox[0],
&_config_octa_x[0],
&_config_octa_plus[0],
&_config_octa_cox[0],
@@ -158,6 +172,7 @@ const unsigned _config_rotor_count[MultirotorMixer::MAX_GEOMETRY] = {
4, /* quad_wide */
6, /* hex_x */
6, /* hex_plus */
6, /* hex_cox */
8, /* octa_x */
8, /* octa_plus */
8, /* octa_cox */
@@ -171,12 +186,12 @@ MultirotorMixer::MultirotorMixer(ControlCallback control_cb,
float roll_scale,
float pitch_scale,
float yaw_scale,
float deadband) :
float idle_speed) :
Mixer(control_cb, cb_handle),
_roll_scale(roll_scale),
_pitch_scale(pitch_scale),
_yaw_scale(yaw_scale),
_deadband(-1.0f + deadband), /* shift to output range here to avoid runtime calculation */
_idle_speed(-1.0f + idle_speed * 2.0f), /* shift to output range here to avoid runtime calculation */
_rotor_count(_config_rotor_count[geometry]),
_rotors(_config_index[geometry])
{
@@ -247,6 +262,9 @@ MultirotorMixer::from_text(Mixer::ControlCallback control_cb, uintptr_t cb_handl
} else if (!strcmp(geomname, "6x")) {
geometry = MultirotorMixer::HEX_X;
} else if (!strcmp(geomname, "6c")) {
geometry = MultirotorMixer::HEX_COX;
} else if (!strcmp(geomname, "8+")) {
geometry = MultirotorMixer::OCTA_PLUS;
@@ -276,67 +294,67 @@ MultirotorMixer::from_text(Mixer::ControlCallback control_cb, uintptr_t cb_handl
unsigned
MultirotorMixer::mix(float *outputs, unsigned space)
{
float roll = get_control(0, 0) * _roll_scale;
float roll = constrain(get_control(0, 0) * _roll_scale, -1.0f, 1.0f);
//lowsyslog("roll: %d, get_control0: %d, %d\n", (int)(roll), (int)(get_control(0, 0)), (int)(_roll_scale));
float pitch = get_control(0, 1) * _pitch_scale;
float yaw = get_control(0, 2) * _yaw_scale;
float thrust = get_control(0, 3);
float pitch = constrain(get_control(0, 1) * _pitch_scale, -1.0f, 1.0f);
float yaw = constrain(get_control(0, 2) * _yaw_scale, -1.0f, 1.0f);
float thrust = constrain(get_control(0, 3), 0.0f, 1.0f);
//lowsyslog("thrust: %d, get_control3: %d\n", (int)(thrust), (int)(get_control(0, 3)));
float max = 0.0f;
float fixup_scale;
float min_out = 0.0f;
float max_out = 0.0f;
float scale_yaw = 1.0f;
/* use an output factor to prevent too strong control signals at low throttle */
float min_thrust = 0.05f;
float max_thrust = 1.0f;
float startpoint_full_control = 0.40f;
float output_factor;
/* keep roll, pitch and yaw control to 0 below min thrust */
if (thrust <= min_thrust) {
output_factor = 0.0f;
/* linearly increase the output factor from 0 to 1 between min_thrust and startpoint_full_control */
} else if (thrust < startpoint_full_control && thrust > min_thrust) {
output_factor = (thrust / max_thrust) / (startpoint_full_control - min_thrust);
/* and then stay at full control */
} else {
output_factor = max_thrust;
}
roll *= output_factor;
pitch *= output_factor;
yaw *= output_factor;
/* perform initial mix pass yielding un-bounded outputs */
/* perform initial mix pass yielding unbounded outputs, ignore yaw */
for (unsigned i = 0; i < _rotor_count; i++) {
float tmp = roll * _rotors[i].roll_scale +
float out = roll * _rotors[i].roll_scale +
pitch * _rotors[i].pitch_scale +
yaw * _rotors[i].yaw_scale +
thrust;
if (tmp > max)
max = tmp;
/* limit yaw if it causes outputs clipping */
if (out >= 0.0f && out < -yaw * _rotors[i].yaw_scale) {
yaw = -out / _rotors[i].yaw_scale;
}
outputs[i] = tmp;
/* calculate min and max output values */
if (out < min_out) {
min_out = out;
}
if (out > max_out) {
max_out = out;
}
outputs[i] = out;
}
/* scale values into the -1.0 - 1.0 range */
if (max > 1.0f) {
fixup_scale = 2.0f / max;
/* scale down roll/pitch controls if some outputs are negative, don't add yaw, keep total thrust */
if (min_out < 0.0) {
float scale_in = thrust / (thrust - min_out);
/* mix again with adjusted controls */
for (unsigned i = 0; i < _rotor_count; i++) {
outputs[i] = scale_in * (roll * _rotors[i].roll_scale + pitch * _rotors[i].pitch_scale) + thrust;
}
} else {
fixup_scale = 2.0f;
/* roll/pitch mixed without limiting, add yaw control */
for (unsigned i = 0; i < _rotor_count; i++) {
outputs[i] += yaw * _rotors[i].yaw_scale;
}
}
for (unsigned i = 0; i < _rotor_count; i++)
outputs[i] = -1.0f + (outputs[i] * fixup_scale);
/* scale down all outputs if some outputs are too large, reduce total thrust */
float scale_out;
if (max_out > 1.0f) {
scale_out = 1.0f / max_out;
/* ensure outputs are out of the deadband */
for (unsigned i = 0; i < _rotor_count; i++)
if (outputs[i] < _deadband)
outputs[i] = _deadband;
} else {
scale_out = 1.0f;
}
/* scale outputs to range _idle_speed..1, and do final limiting */
for (unsigned i = 0; i < _rotor_count; i++) {
outputs[i] = constrain(_idle_speed + (outputs[i] * (1.0f - _idle_speed) * scale_out), _idle_speed, 1.0f);
}
return _rotor_count;
}
+12 -3
View File
@@ -52,6 +52,15 @@ set hex_plus {
120 CW
}
set hex_cox {
60 CW
60 CCW
180 CW
180 CCW
-60 CW
-60 CCW
}
set octa_x {
22.5 CW
-157.5 CW
@@ -85,7 +94,7 @@ set octa_cox {
-135 CW
}
set tables {quad_x quad_plus quad_v quad_wide hex_x hex_plus octa_x octa_plus octa_cox}
set tables {quad_x quad_plus quad_v quad_wide hex_x hex_plus hex_cox octa_x octa_plus octa_cox}
proc factors {a d} { puts [format "\t{ %9.6f, %9.6f, %5.2f }," [rcos [expr $a + 90]] [rcos $a] [expr -$d]]}
@@ -104,13 +113,13 @@ foreach table $tables {
puts "};"
}
puts "const MultirotorMixer::Rotor *_config_index\[MultirotorMixer::Geometry::MAX_GEOMETRY\] = {"
puts "const MultirotorMixer::Rotor *_config_index\[MultirotorMixer::MAX_GEOMETRY\] = {"
foreach table $tables {
puts [format "\t&_config_%s\[0\]," $table]
}
puts "};"
puts "const unsigned _config_rotor_count\[MultirotorMixer::Geometry::MAX_GEOMETRY\] = {"
puts "const unsigned _config_rotor_count\[MultirotorMixer::MAX_GEOMETRY\] = {"
foreach table $tables {
upvar #0 $table angles
puts [format "\t%u, /* %s */" [expr [llength $angles] / 2] $table]
+3 -61
View File
@@ -521,73 +521,15 @@ param_save_default(void)
return ERROR;
}
if (res == OK) {
res = param_export(fd, false);
res = param_export(fd, false);
if (res != OK) {
warnx("failed to write parameters to file: %s", filename);
}
if (res != OK) {
warnx("failed to write parameters to file: %s", filename);
}
close(fd);
return res;
#if 0
const char *filename_tmp = malloc(strlen(filename) + 5);
sprintf(filename_tmp, "%s.tmp", filename);
/* delete temp file if exist */
res = unlink(filename_tmp);
if (res != OK && errno == ENOENT)
res = OK;
if (res != OK)
warn("failed to delete temp file: %s", filename_tmp);
if (res == OK) {
/* write parameters to temp file */
fd = open(filename_tmp, O_WRONLY | O_CREAT | O_EXCL);
if (fd < 0) {
warn("failed to open temp file: %s", filename_tmp);
res = ERROR;
}
if (res == OK) {
res = param_export(fd, false);
if (res != OK)
warnx("failed to write parameters to file: %s", filename_tmp);
}
close(fd);
}
if (res == OK) {
/* delete parameters file */
res = unlink(filename);
if (res != OK && errno == ENOENT)
res = OK;
if (res != OK)
warn("failed to delete parameters file: %s", filename);
}
if (res == OK) {
/* rename temp file to parameters */
res = rename(filename_tmp, filename);
if (res != OK)
warn("failed to rename %s to %s", filename_tmp, filename);
}
free(filename_tmp);
return res;
#endif
}
/**
+11 -5
View File
@@ -281,13 +281,19 @@ perf_reset(perf_counter_t handle)
void
perf_print_counter(perf_counter_t handle)
{
perf_print_counter_fd(0, handle);
}
void
perf_print_counter_fd(int fd, perf_counter_t handle)
{
if (handle == NULL)
return;
switch (handle->type) {
case PC_COUNT:
printf("%s: %llu events\n",
dprintf(fd, "%s: %llu events\n",
handle->name,
((struct perf_ctr_count *)handle)->event_count);
break;
@@ -295,7 +301,7 @@ perf_print_counter(perf_counter_t handle)
case PC_ELAPSED: {
struct perf_ctr_elapsed *pce = (struct perf_ctr_elapsed *)handle;
printf("%s: %llu events, %lluus elapsed, %llu avg, min %lluus max %lluus\n",
dprintf(fd, "%s: %llu events, %lluus elapsed, %llu avg, min %lluus max %lluus\n",
handle->name,
pce->event_count,
pce->time_total,
@@ -308,7 +314,7 @@ perf_print_counter(perf_counter_t handle)
case PC_INTERVAL: {
struct perf_ctr_interval *pci = (struct perf_ctr_interval *)handle;
printf("%s: %llu events, %llu avg, min %lluus max %lluus\n",
dprintf(fd, "%s: %llu events, %llu avg, min %lluus max %lluus\n",
handle->name,
pci->event_count,
(pci->time_last - pci->time_first) / pci->event_count,
@@ -349,12 +355,12 @@ perf_event_count(perf_counter_t handle)
}
void
perf_print_all(void)
perf_print_all(int fd)
{
perf_counter_t handle = (perf_counter_t)sq_peek(&perf_counters);
while (handle != NULL) {
perf_print_counter(handle);
perf_print_counter_fd(fd, handle);
handle = (perf_counter_t)sq_next(&handle->link);
}
}
+13 -3
View File
@@ -121,16 +121,26 @@ __EXPORT extern void perf_cancel(perf_counter_t handle);
__EXPORT extern void perf_reset(perf_counter_t handle);
/**
* Print one performance counter.
* Print one performance counter to stdout
*
* @param handle The counter to print.
*/
__EXPORT extern void perf_print_counter(perf_counter_t handle);
/**
* Print all of the performance counters.
* Print one performance counter to a fd.
*
* @param fd File descriptor to print to - e.g. 0 for stdout
* @param handle The counter to print.
*/
__EXPORT extern void perf_print_all(void);
__EXPORT extern void perf_print_counter_fd(int fd, perf_counter_t handle);
/**
* Print all of the performance counters.
*
* @param fd File descriptor to print to - e.g. 0 for stdout
*/
__EXPORT extern void perf_print_all(int fd);
/**
* Reset all of the performance counters.
+1 -1
View File
@@ -53,7 +53,7 @@
#define SIGMA 0.000001f
__EXPORT void pid_init(PID_t *pid, uint8_t mode, float dt_min)
__EXPORT void pid_init(PID_t *pid, pid_mode_t mode, float dt_min)
{
pid->mode = mode;
pid->dt_min = dt_min;
@@ -136,12 +136,26 @@ void pwm_limit_calc(const bool armed, const unsigned num_channels, const uint16_
}
effective_pwm[i] = output[i] * (max_pwm[i] - ramp_min_pwm)/2 + (max_pwm[i] + ramp_min_pwm)/2;
/* last line of defense against invalid inputs */
if (effective_pwm[i] < ramp_min_pwm) {
effective_pwm[i] = ramp_min_pwm;
} else if (effective_pwm[i] > max_pwm[i]) {
effective_pwm[i] = max_pwm[i];
}
}
}
break;
case PWM_LIMIT_STATE_ON:
for (unsigned i=0; i<num_channels; i++) {
effective_pwm[i] = output[i] * (max_pwm[i] - min_pwm[i])/2 + (max_pwm[i] + min_pwm[i])/2;
/* last line of defense against invalid inputs */
if (effective_pwm[i] < min_pwm[i]) {
effective_pwm[i] = min_pwm[i];
} else if (effective_pwm[i] > max_pwm[i]) {
effective_pwm[i] = max_pwm[i];
}
}
break;
default:
+1 -1
View File
@@ -140,7 +140,7 @@ int rc_calibration_check(int mavlink_fd) {
/* sanity checks pass, enable channel */
if (count) {
mavlink_log_critical(mavlink_fd, "ERROR: %d config error(s) for RC channel %d.", count, (i + 1));
warnx(mavlink_fd, "ERROR: %d config error(s) for RC channel %d.", count, (i + 1));
warnx("ERROR: %d config error(s) for RC channel %d.", count, (i + 1));
usleep(100000);
}