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commander, navigator, mc_att_control, mc_pos_control: code style fixed

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This commit is contained in:
Anton Babushkin
2014-02-01 11:14:21 +01:00
parent 542ec2d91d
commit 8897894b19
6 changed files with 50 additions and 20 deletions
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src/modules/mc_pos_control/mc_pos_control_main.cpp
+10 -1
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@@ -479,9 +479,11 @@ MulticopterPositionControl::select_alt(bool global)
{
if (global != _use_global_alt) {
_use_global_alt = global;
if (global) {
/* switch from barometric to global altitude */
_alt_sp += _global_pos.alt - _global_pos.baro_alt;
} else {
/* switch from global to barometric altitude */
_alt_sp += _global_pos.baro_alt - _global_pos.alt;
@@ -589,6 +591,7 @@ MulticopterPositionControl::task_main()
if (_control_mode.flag_control_manual_enabled) {
/* select altitude source and update setpoint */
select_alt(_global_pos.global_valid);
if (!_use_global_alt) {
alt = _global_pos.baro_alt;
}
@@ -845,9 +848,10 @@ MulticopterPositionControl::task_main()
/* adjust limits for landing mode */
if (!_control_mode.flag_control_manual_enabled && _pos_sp_triplet.current.valid &&
_pos_sp_triplet.current.type == SETPOINT_TYPE_LAND) {
_pos_sp_triplet.current.type == SETPOINT_TYPE_LAND) {
/* limit max tilt and min lift when landing */
tilt_max = _params.land_tilt_max;
if (thr_min < 0.0f)
thr_min = 0.0f;
}
@@ -863,9 +867,11 @@ MulticopterPositionControl::task_main()
if (thr_min >= 0.0f && tilt_max < M_PI / 2 - 0.05f) {
/* absolute horizontal thrust */
float thrust_sp_xy_len = math::Vector<2>(thrust_sp(0), thrust_sp(1)).length();
if (thrust_sp_xy_len > 0.01f) {
/* max horizontal thrust for given vertical thrust*/
float thrust_xy_max = -thrust_sp(2) * tanf(tilt_max);
if (thrust_sp_xy_len > thrust_xy_max) {
float k = thrust_xy_max / thrust_sp_xy_len;
thrust_sp(0) *= k;
@@ -874,15 +880,18 @@ MulticopterPositionControl::task_main()
}
}
}
} else {
/* thrust compensation for altitude only control mode */
float att_comp;
if (_att.R[2][2] > TILT_COS_MAX) {
att_comp = 1.0f / _att.R[2][2];
} else if (_att.R[2][2] > 0.0f) {
att_comp = ((1.0f / TILT_COS_MAX - 1.0f) / TILT_COS_MAX) * _att.R[2][2] + 1.0f;
saturation_z = true;
} else {
att_comp = 1.0f;
saturation_z = true;