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Fix #8579

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Fan speed code fell into a curly brace
This commit is contained in:
Scott Lahteine 2017-11-28 16:09:37 -06:00
parent ddab1533c5
commit dfcef11bca
1 changed files with 65 additions and 73 deletions
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92
Marlin/planner.cpp
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@ -410,21 +410,58 @@ void Planner::check_axes_activity() {
#if ENABLED(BARICUDA) #if ENABLED(BARICUDA)
#if HAS_HEATER_1 #if HAS_HEATER_1
uint8_t tail_valve_pressure; uint8_t tail_valve_pressure = baricuda_valve_pressure;
#endif #endif
#if HAS_HEATER_2 #if HAS_HEATER_2
uint8_t tail_e_to_p_pressure; uint8_t tail_e_to_p_pressure = baricuda_e_to_p_pressure;
#endif #endif
#endif #endif
#if FAN_COUNT > 0
for (uint8_t i = 0; i < FAN_COUNT; i++) tail_fan_speed[i] = fanSpeeds[i];
#endif
if (blocks_queued()) { if (blocks_queued()) {
#if FAN_COUNT > 0 #if FAN_COUNT > 0
for (uint8_t i = 0; i < FAN_COUNT; i++) for (uint8_t i = 0; i < FAN_COUNT; i++)
tail_fan_speed[i] = block_buffer[block_buffer_tail].fan_speed[i]; tail_fan_speed[i] = block_buffer[block_buffer_tail].fan_speed[i];
#endif
#ifdef FAN_KICKSTART_TIME block_t* block;
#if ENABLED(BARICUDA)
block = &block_buffer[block_buffer_tail];
#if HAS_HEATER_1
tail_valve_pressure = block->valve_pressure;
#endif
#if HAS_HEATER_2
tail_e_to_p_pressure = block->e_to_p_pressure;
#endif
#endif
for (uint8_t b = block_buffer_tail; b != block_buffer_head; b = next_block_index(b)) {
block = &block_buffer[b];
LOOP_XYZE(i) if (block->steps[i]) axis_active[i]++;
}
}
#if ENABLED(DISABLE_X)
if (!axis_active[X_AXIS]) disable_X();
#endif
#if ENABLED(DISABLE_Y)
if (!axis_active[Y_AXIS]) disable_Y();
#endif
#if ENABLED(DISABLE_Z)
if (!axis_active[Z_AXIS]) disable_Z();
#endif
#if ENABLED(DISABLE_E)
if (!axis_active[E_AXIS]) disable_e_steppers();
#endif
#if FAN_COUNT > 0
#if FAN_KICKSTART_TIME > 0
static millis_t fan_kick_end[FAN_COUNT] = { 0 }; static millis_t fan_kick_end[FAN_COUNT] = { 0 };
@ -448,7 +485,7 @@ void Planner::check_axes_activity() {
KICKSTART_FAN(2); KICKSTART_FAN(2);
#endif #endif
#endif // FAN_KICKSTART_TIME #endif // FAN_KICKSTART_TIME > 0
#ifdef FAN_MIN_PWM #ifdef FAN_MIN_PWM
#define CALC_FAN_SPEED(f) (tail_fan_speed[f] ? ( FAN_MIN_PWM + (tail_fan_speed[f] * (255 - FAN_MIN_PWM)) / 255 ) : 0) #define CALC_FAN_SPEED(f) (tail_fan_speed[f] ? ( FAN_MIN_PWM + (tail_fan_speed[f] * (255 - FAN_MIN_PWM)) / 255 ) : 0)
@ -480,51 +517,6 @@ void Planner::check_axes_activity() {
#endif // FAN_COUNT > 0 #endif // FAN_COUNT > 0
block_t* block;
#if ENABLED(BARICUDA)
block = &block_buffer[block_buffer_tail];
#if HAS_HEATER_1
tail_valve_pressure = block->valve_pressure;
#endif
#if HAS_HEATER_2
tail_e_to_p_pressure = block->e_to_p_pressure;
#endif
#endif
for (uint8_t b = block_buffer_tail; b != block_buffer_head; b = next_block_index(b)) {
block = &block_buffer[b];
LOOP_XYZE(i) if (block->steps[i]) axis_active[i]++;
}
}
else {
#if FAN_COUNT > 0
for (uint8_t i = 0; i < FAN_COUNT; i++) tail_fan_speed[i] = fanSpeeds[i];
#endif
#if ENABLED(BARICUDA)
#if HAS_HEATER_1
tail_valve_pressure = baricuda_valve_pressure;
#endif
#if HAS_HEATER_2
tail_e_to_p_pressure = baricuda_e_to_p_pressure;
#endif
#endif
}
#if ENABLED(DISABLE_X)
if (!axis_active[X_AXIS]) disable_X();
#endif
#if ENABLED(DISABLE_Y)
if (!axis_active[Y_AXIS]) disable_Y();
#endif
#if ENABLED(DISABLE_Z)
if (!axis_active[Z_AXIS]) disable_Z();
#endif
#if ENABLED(DISABLE_E)
if (!axis_active[E_AXIS]) disable_e_steppers();
#endif
#if ENABLED(AUTOTEMP) #if ENABLED(AUTOTEMP)
getHighESpeed(); getHighESpeed();
#endif #endif