New multirotor mixer; builds, not yet tested.

This commit is contained in:
px4dev
2012-08-15 00:46:15 -07:00
parent 3edd6c86f2
commit 5198a9daf7
7 changed files with 361 additions and 30 deletions
+11
View File
@@ -59,6 +59,17 @@ Mixer::Mixer(ControlCallback control_cb, uintptr_t cb_handle) :
{
}
float
Mixer::get_control(uint8_t group, uint8_t index)
{
float value;
_control_cb(_cb_handle, group, index, value);
return value;
}
float
Mixer::scale(const mixer_scaler_s &scaler, float input)
{
+61 -6
View File
@@ -184,6 +184,15 @@ protected:
ControlCallback _control_cb;
uintptr_t _cb_handle;
/**
* Invoke the client callback to fetch a control value.
*
* @param group Control group to fetch from.
* @param index Control index to fetch.
* @return The control value.
*/
float get_control(uint8_t group, uint8_t index);
/**
* Perform simpler linear scaling.
*
@@ -328,7 +337,7 @@ private:
};
/**
* Multi-rotor mixer.
* Multi-rotor mixer for pre-defined vehicle geometries.
*
* Collects four inputs (roll, pitch, yaw, thrust) and mixes them to
* a set of outputs based on the configured geometry.
@@ -336,22 +345,68 @@ private:
class __EXPORT MultirotorMixer : public Mixer
{
public:
/**
* Supported multirotor geometries.
*
* XXX add more
*/
enum Geometry {
MULTIROTOR_QUAD_PLUS,
MULTIROTOR_QUAD_X
/* XXX add more here */
QUAD_X = 0, /**< quad in X configuration */
QUAD_PLUS, /**< quad in + configuration */
HEX_X, /**< hex in X configuration */
HEX_PLUS, /**< hex in + configuration */
OCTA_X,
OCTA_PLUS,
MAX_GEOMETRY
};
/**
* Precalculated rotor mix.
*/
struct Rotor {
float roll_scale; /**< scales roll for this rotor */
float pitch_scale; /**< scales pitch for this rotor */
float yaw_scale; /**< scales yaw for this rotor */
};
/**
* Constructor.
*
* @param control_cb Callback invoked to read inputs.
* @param cb_handle Passed to control_cb.
* @param geometry The selected geometry.
* @param roll_scale Scaling factor applied to roll inputs
* compared to thrust.
* @param pitch_scale Scaling factor applied to pitch inputs
* compared to thrust.
* @param yaw_wcale Scaling factor applied to yaw inputs compared
* to thrust.
* @param deadband Minumum rotor control output value; usually
* tuned to ensure that rotors never stall at the
* low end of their control range.
*/
MultirotorMixer(ControlCallback control_cb,
uintptr_t cb_handle,
Geometry geom);
Geometry geometry,
float roll_scale,
float pitch_scale,
float yaw_scale,
float deadband);
~MultirotorMixer();
virtual unsigned mix(float *outputs, unsigned space);
virtual void groups_required(uint32_t &groups);
private:
Geometry _geometry;
float _roll_scale;
float _pitch_scale;
float _yaw_scale;
float _deadband;
unsigned _rotor_count;
const Rotor *_rotors;
};
#endif
+46
View File
@@ -210,6 +210,45 @@ fail:
return nullptr;
}
MultirotorMixer *
mixer_load_multirotor(Mixer::ControlCallback control_cb, uintptr_t cb_handle, const char *buf)
{
MultirotorMixer::Geometry geometry;
char geomname[8];
int s[4];
if (sscanf(buf, "R: %7s %d %d %d %d", geomname, &s[0], &s[1], &s[2], &s[3]) != 5) {
debug("multirotor parse failed on '%s'", buf);
return nullptr;
}
if (!strcmp(geomname, "4+")) {
geometry = MultirotorMixer::QUAD_PLUS;
} else if (!strcmp(geomname, "4x")) {
geometry = MultirotorMixer::QUAD_X;
} else if (!strcmp(geomname, "6+")) {
geometry = MultirotorMixer::HEX_PLUS;
} else if (!strcmp(geomname, "6x")) {
geometry = MultirotorMixer::HEX_X;
} else if (!strcmp(geomname, "8+")) {
geometry = MultirotorMixer::OCTA_PLUS;
} else if (!strcmp(geomname, "8x")) {
geometry = MultirotorMixer::OCTA_X;
} else {
debug("unrecognised geometry '%s'", geomname);
return nullptr;
}
return new MultirotorMixer(
control_cb,
cb_handle,
geometry,
s[0] / 10000.0f,
s[1] / 10000.0f,
s[2] / 10000.0f,
s[3] / 10000.0f);
}
int
mixer_load(Mixer::ControlCallback control_cb, uintptr_t cb_handle, int fd, Mixer *&mixer)
{
@@ -239,6 +278,13 @@ mixer_load(Mixer::ControlCallback control_cb, uintptr_t cb_handle, int fd, Mixer
return (mixer == nullptr) ? -1 : 1;
}
/* is it a multirotor mixer? */
if (buf[0] == 'R') {
debug("got a multirotor mixer");
mixer = mixer_load_multirotor(control_cb, cb_handle, buf);
return (mixer == nullptr) ? -1 : 1;
}
/* we don't recognise the mixer type */
debug("unrecognized mixer type '%c'", buf[0]);
return -1;
+120 -3
View File
@@ -50,14 +50,100 @@
#include <stdio.h>
#include <math.h>
#include <unistd.h>
#include <math.h>
#include "mixer.h"
#define CW (-1.0f)
#define CCW (1.0f)
namespace
{
/*
* These tables automatically generated by multi_tables - do not edit.
*/
const MultirotorMixer::Rotor _config_quad_x[] = {
{ -0.707107, 0.707107, 1.00 },
{ 0.707107, -0.707107, 1.00 },
{ 0.707107, 0.707107, -1.00 },
{ -0.707107, -0.707107, -1.00 },
};
const MultirotorMixer::Rotor _config_quad_plus[] = {
{ -1.000000, 0.000000, 1.00 },
{ 1.000000, 0.000000, 1.00 },
{ 0.000000, 1.000000, -1.00 },
{ -0.000000, -1.000000, -1.00 },
};
const MultirotorMixer::Rotor _config_hex_x[] = {
{ -1.000000, 0.000000, -1.00 },
{ 1.000000, 0.000000, 1.00 },
{ 0.500000, 0.866025, -1.00 },
{ -0.500000, -0.866025, 1.00 },
{ -0.500000, 0.866025, 1.00 },
{ 0.500000, -0.866025, -1.00 },
};
const MultirotorMixer::Rotor _config_hex_plus[] = {
{ 0.000000, 1.000000, -1.00 },
{ -0.000000, -1.000000, 1.00 },
{ 0.866025, -0.500000, -1.00 },
{ -0.866025, 0.500000, 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 },
{ -0.923880, 0.382683, 1.00 },
{ -0.382683, -0.923880, 1.00 },
{ 0.382683, 0.923880, 1.00 },
{ 0.923880, -0.382683, 1.00 },
{ 0.923880, 0.382683, -1.00 },
{ -0.923880, -0.382683, -1.00 },
};
const MultirotorMixer::Rotor _config_octa_plus[] = {
{ 0.000000, 1.000000, -1.00 },
{ -0.000000, -1.000000, -1.00 },
{ -0.707107, 0.707107, 1.00 },
{ -0.707107, -0.707107, 1.00 },
{ 0.707107, 0.707107, 1.00 },
{ 0.707107, -0.707107, 1.00 },
{ 1.000000, 0.000000, -1.00 },
{ -1.000000, 0.000000, -1.00 },
};
const MultirotorMixer::Rotor *_config_index[MultirotorMixer::Geometry::MAX_GEOMETRY] = {
&_config_quad_x[0],
&_config_quad_plus[0],
&_config_hex_x[0],
&_config_hex_plus[0],
&_config_octa_x[0],
&_config_octa_plus[0],
};
const unsigned _config_rotor_count[MultirotorMixer::Geometry::MAX_GEOMETRY] = {
4, /* quad_x */
4, /* quad_plus */
6, /* hex_x */
6, /* hex_plus */
8, /* octa_x */
8, /* octa_plus */
};
}
MultirotorMixer::MultirotorMixer(ControlCallback control_cb,
uintptr_t cb_handle,
MultirotorMixer::Geometry geom) :
Geometry geometry,
float roll_scale,
float pitch_scale,
float yaw_scale,
float deadband) :
Mixer(control_cb, cb_handle),
_geometry(geom)
_roll_scale(roll_scale),
_pitch_scale(pitch_scale),
_yaw_scale(yaw_scale),
_deadband(-1.0 + deadband), /* shift to output range here to avoid runtime calculation */
_rotor_count(_config_rotor_count[geometry]),
_rotors(_config_index[geometry])
{
}
@@ -68,7 +154,38 @@ MultirotorMixer::~MultirotorMixer()
unsigned
MultirotorMixer::mix(float *outputs, unsigned space)
{
/* XXX implement this */
float roll = get_control(0, 0) * _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 max = 0.0f;
float fixup_scale;
/* perform initial mix pass yielding un-bounded outputs */
for (unsigned i = 0; i < _rotor_count; i++) {
float tmp = roll * _rotors[i].roll_scale +
pitch * _rotors[i].pitch_scale +
yaw * _rotors[i].yaw_scale +
thrust;
if (tmp > max)
max = tmp;
outputs[i] = tmp;
}
/* scale values into the -1.0 - 1.0 range */
if (max > 1.0f) {
fixup_scale = 2.0f / max;
} else {
fixup_scale = 2.0f;
}
for (unsigned i = 0; i < _rotor_count; i++)
outputs[i] *= -1.0 + (outputs[i] * fixup_scale);
/* ensure outputs are out of the deadband */
for (unsigned i = 0; i < _rotor_count; i++)
if (outputs[i] < _deadband)
outputs[i] = _deadband;
return 0;
}
+93
View File
@@ -0,0 +1,93 @@
#!/usr/bin/tclsh
#
# Generate multirotor mixer scale tables compatible with the ArduCopter layout
#
proc rad {a} { expr ($a / 360.0) * 2 * acos(-1) }
proc rcos {a} { expr cos([rad $a])}
set quad_x {
45 CCW
-135 CCW
-45 CW
135 CW
}
set quad_plus {
90 CCW
-90 CCW
0 CW
180 CW
}
set hex_x {
90 CW
-90 CCW
-30 CW
150 CCW
30 CCW
-150 CW
}
set hex_plus {
0 CW
180 CCW
-120 CW
60 CCW
-60 CCW
120 CW
}
set octa_x {
22.5 CW
-157.5 CW
67.5 CCW
157.5 CCW
-22.5 CCW
-112.5 CCW
-67.5 CW
112.5 CW
}
set octa_plus {
0 CW
180 CW
45 CCW
135 CCW
-45 CCW
-135 CCW
-90 CW
90 CW
}
set tables {quad_x quad_plus 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] $d]}
foreach table $tables {
puts [format "const MultirotorMixer::Rotor _config_%s\[\] = {" $table]
upvar #0 $table angles
foreach {angle dir} $angles {
if {$dir == "CW"} {
set dd -1.0
} else {
set dd 1.0
}
factors $angle $dd
}
puts "};"
}
puts "const MultirotorMixer::Rotor *_config_index\[MultirotorMixer::Geometry::MAX_GEOMETRY\] = {"
foreach table $tables {
puts [format "\t&_config_%s\[0\]," $table]
}
puts "};"
puts "const unsigned _config_rotor_count\[MultirotorMixer::Geometry::MAX_GEOMETRY\] = {"
foreach table $tables {
upvar #0 $table angles
puts [format "\t%u, /* %s */" [expr [llength $angles] / 2] $table]
}
puts "};"