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| author | Julian Oes <julian@oes.ch> | 2013-08-15 14:04:46 +0200 |
|---|---|---|
| committer | Julian Oes <julian@oes.ch> | 2013-08-15 14:04:46 +0200 |
| commit | 56575eb068879beb68b3730ca6d3bb3755d6960a (patch) | |
| tree | 1b7b4c028c2b936db81310e82a8ef84adc125e3d /src/modules/fixedwing_att_control/fixedwing_att_control_att.c | |
| parent | 50cf1c01b701fced6437dfe574fd09cd312b9f15 (diff) | |
| parent | 561ec495b7df5b3ff4536d16d1389d1f02affd06 (diff) | |
| download | px4-firmware-56575eb068879beb68b3730ca6d3bb3755d6960a.tar.gz px4-firmware-56575eb068879beb68b3730ca6d3bb3755d6960a.tar.bz2 px4-firmware-56575eb068879beb68b3730ca6d3bb3755d6960a.zip | |
Merge remote-tracking branch 'px4/new_state_machine_drton' into fmuv2_bringup_new_state_machine_drton
Conflicts:
src/drivers/blinkm/blinkm.cpp
src/drivers/px4io/px4io.cpp
src/modules/commander/state_machine_helper.c
src/modules/px4iofirmware/protocol.h
src/modules/px4iofirmware/registers.c
src/modules/systemlib/systemlib.h
src/systemcmds/reboot/reboot.c
Diffstat (limited to 'src/modules/fixedwing_att_control/fixedwing_att_control_att.c')
| -rw-r--r-- | src/modules/fixedwing_att_control/fixedwing_att_control_att.c | 4 |
1 files changed, 2 insertions, 2 deletions
diff --git a/src/modules/fixedwing_att_control/fixedwing_att_control_att.c b/src/modules/fixedwing_att_control/fixedwing_att_control_att.c index 2aeca3a98..68c176459 100644 --- a/src/modules/fixedwing_att_control/fixedwing_att_control_att.c +++ b/src/modules/fixedwing_att_control/fixedwing_att_control_att.c @@ -142,7 +142,7 @@ int fixedwing_att_control_attitude(const struct vehicle_attitude_setpoint_s *att } /* Roll (P) */ - rates_sp->roll = pid_calculate(&roll_controller, att_sp->roll_body, att->roll, 0, 0); + rates_sp->roll = pid_calculate(&roll_controller, att_sp->roll_body, att->roll, 0, 0, NULL, NULL, NULL); /* Pitch (P) */ @@ -152,7 +152,7 @@ int fixedwing_att_control_attitude(const struct vehicle_attitude_setpoint_s *att /* set pitch plus feedforward roll compensation */ rates_sp->pitch = pid_calculate(&pitch_controller, att_sp->pitch_body + pitch_sp_rollcompensation, - att->pitch, 0, 0); + att->pitch, 0, 0, NULL, NULL, NULL); /* Yaw (from coordinated turn constraint or lateral force) */ rates_sp->yaw = (att->rollspeed * rates_sp->roll + 9.81f * sinf(att->roll) * cosf(att->pitch) + speed_body[0] * rates_sp->pitch * sinf(att->roll)) |