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Commit f8e291da authored by Daniel Agar's avatar Daniel Agar Committed by GitHub
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mavlink VFR_HUD throttle use first 2 groups (#7106)

- fixes #6974
parent e9aef2eb
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......@@ -970,8 +970,11 @@ private:
MavlinkOrbSubscription *_armed_sub;
uint64_t _armed_time;
MavlinkOrbSubscription *_act_sub;
uint64_t _act_time;
MavlinkOrbSubscription *_act0_sub;
uint64_t _act0_time;
MavlinkOrbSubscription *_act1_sub;
uint64_t _act1_time;
MavlinkOrbSubscription *_airspeed_sub;
uint64_t _airspeed_time;
......@@ -991,8 +994,10 @@ protected:
_pos_time(0),
_armed_sub(_mavlink->add_orb_subscription(ORB_ID(actuator_armed))),
_armed_time(0),
_act_sub(_mavlink->add_orb_subscription(ORB_ID(actuator_controls_0))),
_act_time(0),
_act0_sub(_mavlink->add_orb_subscription(ORB_ID(actuator_controls_0))),
_act0_time(0),
_act1_sub(_mavlink->add_orb_subscription(ORB_ID(actuator_controls_1))),
_act1_time(0),
_airspeed_sub(_mavlink->add_orb_subscription(ORB_ID(airspeed))),
_airspeed_time(0),
_sensor_sub(_mavlink->add_orb_subscription(ORB_ID(sensor_combined))),
......@@ -1004,14 +1009,16 @@ protected:
struct vehicle_attitude_s att = {};
struct vehicle_global_position_s pos = {};
struct actuator_armed_s armed = {};
struct actuator_controls_s act = {};
struct airspeed_s airspeed = {};
struct actuator_controls_s act0 = {};
struct actuator_controls_s act1 = {};
bool updated = _att_sub->update(&_att_time, &att);
updated |= _pos_sub->update(&_pos_time, &pos);
updated |= _armed_sub->update(&_armed_time, &armed);
updated |= _act_sub->update(&_act_time, &act);
updated |= _airspeed_sub->update(&_airspeed_time, &airspeed);
updated |= _act0_sub->update(&_act0_time, &act0);
updated |= _act1_sub->update(&_act1_time, &act1);
if (updated) {
mavlink_vfr_hud_t msg = {};
......@@ -1019,7 +1026,19 @@ protected:
msg.airspeed = airspeed.indicated_airspeed_m_s;
msg.groundspeed = sqrtf(pos.vel_n * pos.vel_n + pos.vel_e * pos.vel_e);
msg.heading = _wrap_2pi(euler.psi()) * M_RAD_TO_DEG_F;
msg.throttle = armed.armed ? act.control[3] * 100.0f : 0.0f;
if (armed.armed) {
// VFR_HUD throttle should only be used for operator feedback.
// VTOLs switch between actuator_controls_0 and actuator_controls_1. During transition there isn't a
// a single throttle value, but this should still be a useful heuristic for operator awareness.
//
// Use ACTUATOR_CONTROL_TARGET if accurate states are needed.
msg.throttle = 100 * math::max(act0.control[actuator_controls_s::INDEX_THROTTLE],
act1.control[actuator_controls_s::INDEX_THROTTLE]);
} else {
msg.throttle = 0.0f;
}
if (_pos_time > 0) {
/* use global estimate */
......
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