forked from Archive/PX4-Autopilot
fw_att_control: delete the unused flag
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8267bdf4a5
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2db140bcab
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@ -136,7 +136,6 @@ private:
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perf_counter_t _loop_perf; /**< loop performance counter */
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perf_counter_t _loop_perf; /**< loop performance counter */
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bool _setpoint_valid; /**< flag if the position control setpoint is valid */
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bool _setpoint_valid; /**< flag if the position control setpoint is valid */
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bool _airspeed_valid; /**< flag if the airspeed measurement is valid */
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struct {
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struct {
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float tconst;
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float tconst;
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@ -293,8 +292,7 @@ FixedwingAttitudeControl::FixedwingAttitudeControl() :
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/* performance counters */
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/* performance counters */
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_loop_perf(perf_alloc(PC_ELAPSED, "fw att control")),
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_loop_perf(perf_alloc(PC_ELAPSED, "fw att control")),
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/* states */
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/* states */
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_setpoint_valid(false),
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_setpoint_valid(false)
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_airspeed_valid(false)
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{
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{
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/* safely initialize structs */
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/* safely initialize structs */
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_att = {0};
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_att = {0};
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@ -753,10 +751,6 @@ FixedwingAttitudeControl::task_main()
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warnx("Non-finite setpoint roll_sp: %.4f, pitch_sp %.4f", roll_sp, pitch_sp);
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warnx("Non-finite setpoint roll_sp: %.4f, pitch_sp %.4f", roll_sp, pitch_sp);
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}
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}
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// warnx("aspd: %s: %6.2f, aspd scaling: %6.2f, controls: %5.2f %5.2f %5.2f %5.2f", (_airspeed_valid) ? "valid" : "unknown",
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// airspeed, airspeed_scaling, _actuators.control[0], _actuators.control[1],
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// _actuators.control[2], _actuators.control[3]);
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/*
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/*
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* Lazily publish the rate setpoint (for analysis, the actuators are published below)
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* Lazily publish the rate setpoint (for analysis, the actuators are published below)
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* only once available
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* only once available
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