rooty/LibrePilot
1
0
Fork 0
mirror of https://bitbucket.org/librepilot/librepilot.git synced 2025-03-15 07:29:15 +01:00
Code Issues Releases Activity

LP-66 Fixed wing : Roll differential mixing on flight side

Browse Source
This commit is contained in:
Laurent Lalanne 2015-07-29 06:36:22 +02:00
parent 9a886d6d72
commit 31c30d752f
2 changed files with 58 additions and 32 deletions
Show Stats Download Patch File Download Diff File Expand all files Collapse all files

88
flight/modules/Actuator/actuator.c
View File

@ -9,6 +9,7 @@
*
* @file actuator.c
* @author The OpenPilot Team, http://www.openpilot.org Copyright (C) 2010.
* @author The LibrePilot Project, http://www.librepilot.org Copyright (C) 2015.
* @brief Actuator module. Drives the actuators (servos, motors etc).
*
* @see The GNU Public License (GPL) Version 3
@ -110,7 +111,7 @@ static void ActuatorSettingsUpdatedCb(UAVObjEvent *ev);
static void SettingsUpdatedCb(UAVObjEvent *ev);
float ProcessMixer(const int index, const float curve1, const float curve2,
ActuatorDesiredData *desired,
const float period, bool multirotor);
const float period, bool multirotor, bool fixedwing);
// this structure is equivalent to the UAVObjects for one mixer.
typedef struct {
@ -271,6 +272,7 @@ static void actuatorTask(__attribute__((unused)) void *parameters)
bool activeThrottle = (throttleDesired < -0.001f || throttleDesired > 0.001f); // for ground and reversible motors
bool positiveThrottle = (throttleDesired > 0.00f);
bool multirotor = (GetCurrentFrameType() == FRAME_TYPE_MULTIROTOR); // check if frame is a multirotor.
bool fixedwing = (GetCurrentFrameType() == FRAME_TYPE_FIXED_WING); // check if frame is a fixedwing.
bool alwaysArmed = settings.Arming == FLIGHTMODESETTINGS_ARMING_ALWAYSARMED;
bool AlwaysStabilizeWhenArmed = settings.AlwaysStabilizeWhenArmed == FLIGHTMODESETTINGS_ALWAYSSTABILIZEWHENARMED_TRUE;
@ -406,7 +408,7 @@ static void actuatorTask(__attribute__((unused)) void *parameters)
nonreversible_curve2 = 0.0f;
}
}
status[ct] = ProcessMixer(ct, nonreversible_curve1, nonreversible_curve2, &desired, dTSeconds, multirotor);
status[ct] = ProcessMixer(ct, nonreversible_curve1, nonreversible_curve2, &desired, dTSeconds, multirotor, fixedwing);
// If not armed or motors aren't meant to spin all the time
if (!armed ||
(!spinWhileArmed && !positiveThrottle)) {
@ -424,7 +426,7 @@ static void actuatorTask(__attribute__((unused)) void *parameters)
}
}
} else if (mixer_type == MIXERSETTINGS_MIXER1TYPE_REVERSABLEMOTOR) {
status[ct] = ProcessMixer(ct, curve1, curve2, &desired, dTSeconds, multirotor);
status[ct] = ProcessMixer(ct, curve1, curve2, &desired, dTSeconds, multirotor, fixedwing);
// Reversable Motors are like Motors but go to neutral instead of minimum
// If not armed or motor is inactive - no "spinwhilearmed" for this engine type
if (!armed || !activeThrottle) {
@ -433,7 +435,7 @@ static void actuatorTask(__attribute__((unused)) void *parameters)
status[ct] = 0; // force neutral throttle
}
} else if (mixer_type == MIXERSETTINGS_MIXER1TYPE_SERVO) {
status[ct] = ProcessMixer(ct, curve1, curve2, &desired, dTSeconds, multirotor);
status[ct] = ProcessMixer(ct, curve1, curve2, &desired, dTSeconds, multirotor, fixedwing);
} else {
status[ct] = -1;
@ -555,15 +557,35 @@ static void actuatorTask(__attribute__((unused)) void *parameters)
* Process mixing for one actuator
*/
float ProcessMixer(const int index, const float curve1, const float curve2,
ActuatorDesiredData *desired, const float period, bool multirotor)
ActuatorDesiredData *desired, const float period, bool multirotor, bool fixedwing)
{
static float lastFilteredResult[MAX_MIX_ACTUATORS];
const Mixer_t *mixers = (Mixer_t *)&mixerSettings.Mixer1Type; // pointer to array of mixers in UAVObjects
const Mixer_t *mixer = &mixers[index];
float differential = 1.0f;
// Apply differential only for fixedwing and Roll servos
if (fixedwing && (mixerSettings.FirstRollServo > 0) &&
(mixer->type == MIXERSETTINGS_MIXER1TYPE_SERVO) &&
(mixer->matrix[MIXERSETTINGS_MIXER1VECTOR_ROLL] != 0)) {
// Positive differential
if (mixerSettings.RollDifferential > 0) {
// Check for first Roll servo (should be left aileron or elevon) and Roll desired (positive/negative)
if (((index == mixerSettings.FirstRollServo - 1) && (desired->Roll > 0.0f))
|| ((index != mixerSettings.FirstRollServo - 1) && (desired->Roll < 0.0f))) {
differential -= (mixerSettings.RollDifferential * 0.01f);
}
} else if (mixerSettings.RollDifferential < 0) {
if (((index == mixerSettings.FirstRollServo - 1) && (desired->Roll < 0.0f))
|| ((index != mixerSettings.FirstRollServo - 1) && (desired->Roll > 0.0f))) {
differential -= (-mixerSettings.RollDifferential * 0.01f);
}
}
}
float result = ((((float)mixer->matrix[MIXERSETTINGS_MIXER1VECTOR_THROTTLECURVE1]) * curve1) +
(((float)mixer->matrix[MIXERSETTINGS_MIXER1VECTOR_THROTTLECURVE2]) * curve2) +
(((float)mixer->matrix[MIXERSETTINGS_MIXER1VECTOR_ROLL]) * desired->Roll) +
(((float)mixer->matrix[MIXERSETTINGS_MIXER1VECTOR_ROLL]) * desired->Roll * differential) +
(((float)mixer->matrix[MIXERSETTINGS_MIXER1VECTOR_PITCH]) * desired->Pitch) +
(((float)mixer->matrix[MIXERSETTINGS_MIXER1VECTOR_YAW]) * desired->Yaw)) / 128.0f;
@ -575,36 +597,38 @@ float ProcessMixer(const int index, const float curve1, const float curve2,
}
}
// feed forward
float accumulator = filterAccumulator[index];
accumulator += (result - lastResult[index]) * mixerSettings.FeedForward;
lastResult[index] = result;
result += accumulator;
if (period > 0.0f) {
if (accumulator > 0.0f) {
float invFilter = period / mixerSettings.AccelTime;
if (invFilter > 1) {
invFilter = 1;
if (!fixedwing) {
// feed forward, do not apply to fixedwing
float accumulator = filterAccumulator[index];
accumulator += (result - lastResult[index]) * mixerSettings.FeedForward;
lastResult[index] = result;
result += accumulator;
if (period > 0.0f) {
if (accumulator > 0.0f) {
float invFilter = period / mixerSettings.AccelTime;
if (invFilter > 1) {
invFilter = 1;
}
accumulator -= accumulator * invFilter;
} else {
float invFilter = period / mixerSettings.DecelTime;
if (invFilter > 1) {
invFilter = 1;
}
accumulator -= accumulator * invFilter;
}
accumulator -= accumulator * invFilter;
} else {
float invFilter = period / mixerSettings.DecelTime;
if (invFilter > 1) {
invFilter = 1;
}
accumulator -= accumulator * invFilter;
}
}
filterAccumulator[index] = accumulator;
result += accumulator;
filterAccumulator[index] = accumulator;
result += accumulator;
// acceleration limit
float dt = result - lastFilteredResult[index];
float maxDt = mixerSettings.MaxAccel * period;
if (dt > maxDt) { // we are accelerating too hard
result = lastFilteredResult[index] + maxDt;
// acceleration limit
float dt = result - lastFilteredResult[index];
float maxDt = mixerSettings.MaxAccel * period;
if (dt > maxDt) { // we are accelerating too hard
result = lastFilteredResult[index] + maxDt;
}
lastFilteredResult[index] = result;
}
lastFilteredResult[index] = result;
}
return result;

2
shared/uavobjectdefinition/mixersettings.xml
View File

@ -5,6 +5,8 @@
<field name="MixerValueRoll" units="percent" type="int8" elements="1" defaultvalue="50"/>
<field name="MixerValuePitch" units="percent" type="int8" elements="1" defaultvalue="50"/>
<field name="MixerValueYaw" units="percent" type="int8" elements="1" defaultvalue="50"/>
<field name="RollDifferential" units="percent" type="int8" elements="1" defaultvalue="0"/>
<field name="FirstRollServo" units="" type="uint8" elements="1" defaultvalue="0"/>
<field name="FeedForward" units="" type="float" elements="1" defaultvalue="0"/>
<field name="AccelTime" units="ms" type="float" elements="1" defaultvalue="0"/>
<field name="DecelTime" units="ms" type="float" elements="1" defaultvalue="0"/>