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log secondary attitude and fixed wing controls for VTOL

sbg
Roman Bapst 10 years ago
parent
commit
ad204bbb5d
  1. 25
      src/modules/sdlog2/sdlog2.c
  2. 13
      src/modules/sdlog2/sdlog2_messages.h

25
src/modules/sdlog2/sdlog2.c

@ -941,6 +941,7 @@ int sdlog2_thread_main(int argc, char *argv[]) @@ -941,6 +941,7 @@ int sdlog2_thread_main(int argc, char *argv[])
struct vehicle_rates_setpoint_s rates_sp;
struct actuator_outputs_s act_outputs;
struct actuator_controls_s act_controls;
struct actuator_controls_s act_controls1;
struct vehicle_local_position_s local_pos;
struct vehicle_local_position_setpoint_s local_pos_sp;
struct vehicle_global_position_s global_pos;
@ -981,6 +982,7 @@ int sdlog2_thread_main(int argc, char *argv[]) @@ -981,6 +982,7 @@ int sdlog2_thread_main(int argc, char *argv[])
struct log_LPSP_s log_LPSP;
struct log_GPS_s log_GPS;
struct log_ATTC_s log_ATTC;
struct log_FWC_s log_FWC;
struct log_STAT_s log_STAT;
struct log_RC_s log_RC;
struct log_OUT0_s log_OUT0;
@ -1022,6 +1024,7 @@ int sdlog2_thread_main(int argc, char *argv[]) @@ -1022,6 +1024,7 @@ int sdlog2_thread_main(int argc, char *argv[])
int rates_sp_sub;
int act_outputs_sub;
int act_controls_sub;
int act_controls_1_sub;
int local_pos_sub;
int local_pos_sp_sub;
int global_pos_sub;
@ -1055,6 +1058,7 @@ int sdlog2_thread_main(int argc, char *argv[]) @@ -1055,6 +1058,7 @@ int sdlog2_thread_main(int argc, char *argv[])
subs.rates_sp_sub = orb_subscribe(ORB_ID(vehicle_rates_setpoint));
subs.act_outputs_sub = orb_subscribe(ORB_ID_VEHICLE_CONTROLS);
subs.act_controls_sub = orb_subscribe(ORB_ID_VEHICLE_ATTITUDE_CONTROLS);
subs.act_controls_1_sub = orb_subscribe(ORB_ID(actuator_controls_1));
subs.local_pos_sub = orb_subscribe(ORB_ID(vehicle_local_position));
subs.local_pos_sp_sub = orb_subscribe(ORB_ID(vehicle_local_position_setpoint));
subs.global_pos_sub = orb_subscribe(ORB_ID(vehicle_global_position));
@ -1375,6 +1379,18 @@ int sdlog2_thread_main(int argc, char *argv[]) @@ -1375,6 +1379,18 @@ int sdlog2_thread_main(int argc, char *argv[])
log_msg.body.log_ATT.gy = buf.att.g_comp[1];
log_msg.body.log_ATT.gz = buf.att.g_comp[2];
LOGBUFFER_WRITE_AND_COUNT(ATT);
// secondary attitude
log_msg.msg_type = LOG_ATT2_MSG;
log_msg.body.log_ATT.roll = buf.att.roll_sec;
log_msg.body.log_ATT.pitch = buf.att.pitch_sec;
log_msg.body.log_ATT.yaw = buf.att.yaw_sec;
log_msg.body.log_ATT.roll_rate = buf.att.rollspeed_sec;
log_msg.body.log_ATT.pitch_rate = buf.att.pitchspeed_sec;
log_msg.body.log_ATT.yaw_rate = buf.att.yawspeed_sec;
log_msg.body.log_ATT.gx = buf.att.g_comp_sec[0];
log_msg.body.log_ATT.gy = buf.att.g_comp_sec[1];
log_msg.body.log_ATT.gz = buf.att.g_comp_sec[2];
LOGBUFFER_WRITE_AND_COUNT(ATT);
}
/* --- ATTITUDE SETPOINT --- */
@ -1413,6 +1429,15 @@ int sdlog2_thread_main(int argc, char *argv[]) @@ -1413,6 +1429,15 @@ int sdlog2_thread_main(int argc, char *argv[])
LOGBUFFER_WRITE_AND_COUNT(ATTC);
}
if(copy_if_updated(ORB_ID(actuator_controls_1),subs.act_controls_1_sub,&buf.act_controls1)) {
log_msg.msg_type = LOG_FWC_MSG;
log_msg.body.log_FWC.roll = buf.act_controls1.control[0];
log_msg.body.log_FWC.pitch = buf.act_controls1.control[1];
log_msg.body.log_FWC.yaw = buf.act_controls1.control[2];
log_msg.body.log_FWC.thrust = buf.act_controls1.control[3];
LOGBUFFER_WRITE_AND_COUNT(FWC);
}
/* --- LOCAL POSITION --- */
if (copy_if_updated(ORB_ID(vehicle_local_position), subs.local_pos_sub, &buf.local_pos)) {
log_msg.msg_type = LOG_LPOS_MSG;

13
src/modules/sdlog2/sdlog2_messages.h

@ -50,6 +50,7 @@ @@ -50,6 +50,7 @@
#pragma pack(push, 1)
/* --- ATT - ATTITUDE --- */
#define LOG_ATT_MSG 2
#define LOG_ATT2_MSG 41
struct log_ATT_s {
float roll;
float pitch;
@ -422,6 +423,14 @@ struct log_ENCD_s { @@ -422,6 +423,14 @@ struct log_ENCD_s {
float vel1;
};
/* ATTITUDE CONTROLS (ACTUATOR_1 CONTROLS) */
#define LOG_FWC_MSG 40
struct log_FWC_s {
float roll;
float pitch;
float yaw;
float thrust;
};
/********** SYSTEM MESSAGES, ID > 0x80 **********/
@ -450,7 +459,8 @@ struct log_PARM_s { @@ -450,7 +459,8 @@ struct log_PARM_s {
/* construct list of all message formats */
static const struct log_format_s log_formats[] = {
/* business-level messages, ID < 0x80 */
LOG_FORMAT(ATT, "fffffffff", "Roll,Pitch,Yaw,RollRate,PitchRate,YawRate,GX,GY,GZ"),
LOG_FORMAT_S(ATT, ATT, "fffffffff", "Roll,Pitch,Yaw,RollRate,PitchRate,YawRate,GX,GY,GZ"),
LOG_FORMAT_S(ATT2, ATT, "fffffffff", "Roll,Pitch,Yaw,RollRate,PitchRate,YawRate,GX,GY,GZ"),
LOG_FORMAT(ATSP, "ffff", "RollSP,PitchSP,YawSP,ThrustSP"),
LOG_FORMAT_S(IMU, IMU, "fffffffff", "AccX,AccY,AccZ,GyroX,GyroY,GyroZ,MagX,MagY,MagZ"),
LOG_FORMAT_S(IMU1, IMU, "fffffffff", "AccX,AccY,AccZ,GyroX,GyroY,GyroZ,MagX,MagY,MagZ"),
@ -460,6 +470,7 @@ static const struct log_format_s log_formats[] = { @@ -460,6 +470,7 @@ static const struct log_format_s log_formats[] = {
LOG_FORMAT(LPSP, "ffff", "X,Y,Z,Yaw"),
LOG_FORMAT(GPS, "QBffLLfffffBHHH", "GPSTime,Fix,EPH,EPV,Lat,Lon,Alt,VelN,VelE,VelD,Cog,nSat,SNR,N,J"),
LOG_FORMAT(ATTC, "ffff", "Roll,Pitch,Yaw,Thrust"),
LOG_FORMAT(FWC,"ffff", "Roll,Pitch,Yaw,Thrust"),
LOG_FORMAT(STAT, "BBBfBB", "MainState,ArmState,FailsafeState,BatRem,BatWarn,Landed"),
LOG_FORMAT(RC, "ffffffffBB", "Ch0,Ch1,Ch2,Ch3,Ch4,Ch5,Ch6,Ch7,Count,SignalLost"),
LOG_FORMAT(OUT0, "ffffffff", "Out0,Out1,Out2,Out3,Out4,Out5,Out6,Out7"),

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