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authorLorenz Meier <lm@inf.ethz.ch>2012-08-24 11:40:16 +0200
committerLorenz Meier <lm@inf.ethz.ch>2012-08-24 11:40:42 +0200
commita1b99a3f03a5908ea7e263658343451440326aea (patch)
tree45b3d287c854c99d0655934dbbd4ca65238703b8 /apps/multirotor_att_control
parenta69c55f671b1a2116c0e6c497906844a81ce6c74 (diff)
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Kicked out mix_and_link, deleted old MPU driver, disabled (still needed for reference) old HMC and MS5611 drivers. Removed driver init from up_nsh.c. Reworked fixedwing_control to be closer to up-to-date api, still more clean up needed. Fixed a bug that limited the motor thrust for multirotor control
Diffstat (limited to 'apps/multirotor_att_control')
-rw-r--r--apps/multirotor_att_control/multirotor_att_control_main.c11
1 files changed, 2 insertions, 9 deletions
diff --git a/apps/multirotor_att_control/multirotor_att_control_main.c b/apps/multirotor_att_control/multirotor_att_control_main.c
index 33e7ab7e7..9a23e8290 100644
--- a/apps/multirotor_att_control/multirotor_att_control_main.c
+++ b/apps/multirotor_att_control/multirotor_att_control_main.c
@@ -96,8 +96,6 @@ mc_thread_main(int argc, char *argv[])
memset(&raw, 0, sizeof(raw));
struct ardrone_motors_setpoint_s setpoint;
memset(&setpoint, 0, sizeof(setpoint));
- struct actuator_controls_s actuator_controls;
- memset(&actuator_controls, 0, sizeof(actuator_controls));
struct actuator_controls_s actuators;
struct actuator_armed_s armed;
@@ -153,12 +151,7 @@ mc_thread_main(int argc, char *argv[])
att_sp.yaw_body = 0.0f;
att_sp.thrust = 0.1f;
} else {
- if (state.state_machine == SYSTEM_STATE_MANUAL ||
- state.state_machine == SYSTEM_STATE_GROUND_READY ||
- state.state_machine == SYSTEM_STATE_STABILIZED ||
- state.state_machine == SYSTEM_STATE_AUTO ||
- state.state_machine == SYSTEM_STATE_MISSION_ABORT ||
- state.state_machine == SYSTEM_STATE_EMCY_LANDING) {
+ if (state.flag_system_armed) {
att_sp.thrust = manual.throttle;
armed.armed = true;
@@ -173,7 +166,7 @@ mc_thread_main(int argc, char *argv[])
}
- multirotor_control_attitude(&att_sp, &att, &state, &actuator_controls, motor_test_mode);
+ multirotor_control_attitude(&att_sp, &att, &state, &actuators, motor_test_mode);
/* publish the result */
orb_publish(ORB_ID(actuator_armed), armed_pub, &armed);