fly316/PX4-Autopilot
7
0
Fork 0
mirror of https://gitee.com/mirrors_PX4/PX4-Autopilot.git synced 2026-10-24 01:33:34 +08:00
Code Issues Packages Projects Releases Wiki Activity

updated to master (solved merge conflicts)

Browse Source
This commit is contained in:
Youssef Demitri
2015-10-27 09:26:27 +01:00
parent 560efcbc5b 4241e526aa
commit dd59409e31
289 changed files with 10555 additions and 4461 deletions
Download Patch File Download Diff File Expand all files Collapse all files
src/modules/fw_pos_control_l1/fw_pos_control_l1_params.c
+1 -1
View File
@@ -179,7 +179,7 @@ PARAM_DEFINE_FLOAT(FW_THR_LND_MAX, 1.0f);
* @max 150.0
* @group L1 Control
*/
PARAM_DEFINE_FLOAT(FW_CLMBOUT_DIFF, 25.0f);
PARAM_DEFINE_FLOAT(FW_CLMBOUT_DIFF, 10.0f);
/**
* Maximum climb rate
src/modules/fw_pos_control_l1/mtecs/mTecs.cpp
+11 -11
View File
@@ -53,7 +53,7 @@ mTecs::mTecs() :
_airspeedMin(this, "FW_AIRSPD_MIN", false),
/* Publications */
#if defined(__PX4_NUTTX)
_status(ORB_ID(tecs_status), &getPublications()),
_status(ORB_ID(tecs_status), -1, &getPublications()),
#endif // defined(__PX4_NUTTX)
/* control blocks */
_controlTotalEnergy(this, "THR"),
@@ -88,8 +88,8 @@ int mTecs::updateAltitudeSpeed(float flightPathAngle, float altitude, float alti
float airspeedSp, unsigned mode, LimitOverride limitOverride)
{
/* check if all input arguments are numbers and abort if not so */
if (!isfinite(flightPathAngle) || !isfinite(altitude) ||
!isfinite(altitudeSp) || !isfinite(airspeed) || !isfinite(airspeedSp) || !isfinite(mode)) {
if (!PX4_ISFINITE(flightPathAngle) || !PX4_ISFINITE(altitude) ||
!PX4_ISFINITE(altitudeSp) || !PX4_ISFINITE(airspeed) || !PX4_ISFINITE(airspeedSp) || !PX4_ISFINITE(mode)) {
return -1;
}
@@ -111,8 +111,8 @@ int mTecs::updateAltitudeSpeed(float flightPathAngle, float altitude, float alti
#if defined(__PX4_NUTTX)
/* Write part of the status message */
_status.altitudeSp = altitudeSp;
_status.altitude_filtered = altitudeFiltered;
_status.get().altitudeSp = altitudeSp;
_status.get().altitude_filtered = altitudeFiltered;
#endif // defined(__PX4_NUTTX)
@@ -125,8 +125,8 @@ int mTecs::updateFlightPathAngleSpeed(float flightPathAngle, float flightPathAng
float airspeedSp, unsigned mode, LimitOverride limitOverride)
{
/* check if all input arguments are numbers and abort if not so */
if (!isfinite(flightPathAngle) || !isfinite(flightPathAngleSp) ||
!isfinite(airspeed) || !isfinite(airspeedSp) || !isfinite(mode)) {
if (!PX4_ISFINITE(flightPathAngle) || !PX4_ISFINITE(flightPathAngleSp) ||
!PX4_ISFINITE(airspeed) || !PX4_ISFINITE(airspeedSp) || !PX4_ISFINITE(mode)) {
return -1;
}
@@ -149,8 +149,8 @@ int mTecs::updateFlightPathAngleSpeed(float flightPathAngle, float flightPathAng
#if defined(__PX4_NUTTX)
/* Write part of the status message */
_status.airspeedSp = airspeedSp;
_status.airspeed_filtered = airspeedFiltered;
_status.get().airspeedSp = airspeedSp;
_status.get().airspeed_filtered = airspeedFiltered;
#endif // defined(__PX4_NUTTX)
@@ -163,8 +163,8 @@ int mTecs::updateFlightPathAngleAcceleration(float flightPathAngle, float flight
float accelerationLongitudinalSp, unsigned mode, LimitOverride limitOverride)
{
/* check if all input arguments are numbers and abort if not so */
if (!isfinite(flightPathAngle) || !isfinite(flightPathAngleSp) ||
!isfinite(airspeedFiltered) || !isfinite(accelerationLongitudinalSp) || !isfinite(mode)) {
if (!PX4_ISFINITE(flightPathAngle) || !PX4_ISFINITE(flightPathAngleSp) ||
!PX4_ISFINITE(airspeedFiltered) || !PX4_ISFINITE(accelerationLongitudinalSp) || !PX4_ISFINITE(mode)) {
return -1;
}
/* time measurement */