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last few hacks to make standard_vtol pass
- higher airspeed targets
- higher pusher thrust
- higher takeoff attitude (arsp failure test)
in the airspeed failure case, the lowered airspeed reading causes the
controller to want to speed up until the (wrong) airspeed is at the
setpoint, i.e. the real airspeed quite a bit faster. without these
fixes, tecs does a nosedive to regain airspeed, but never becomes fast
enough (with already maxed out pusher thrust). we pervent this with
the first two adaptations, while the last one gives space for the
remaining nosedive.
fix this permanently by:
- ensuring the model makes sense definitely (pusher thrust, mass, aero
properties)
- noticing the failure faster
- adapting tecs so it doesn't nosedive?
- stop sending airspeed in sih
src/modules/simulation/sensor_airspeed_sim/SensorAirspeedSim.cpp
is already doing that. in the sensor failure case (wrong), that implements
the failure, but the SIH one not, giving conflicting data. so switch
it off
- larger acceptance radius
quadx position mode is just not that accurate. is it a control/model
mismatch problem, or a simulation problem?
- wait longer for disarm in test_vtol_rtl
this would fail at large speed factors previously. timing bug or
acceptable small variation?
This commit is contained in:
@@ -61,9 +61,9 @@ param set-default CA_SV_CS1_TYPE 3 # elevator
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param set-default CA_SV_CS2_TRQ_Y 1
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param set-default CA_SV_CS2_TYPE 4 # rudder
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param set-default FW_AIRSPD_MIN 7
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param set-default FW_AIRSPD_TRIM 10
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param set-default FW_AIRSPD_MAX 12
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param set-default FW_AIRSPD_MIN 10
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param set-default FW_AIRSPD_TRIM 15
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param set-default FW_AIRSPD_MAX 20
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param set-default PWM_MAIN_FUNC1 101
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param set-default PWM_MAIN_FUNC2 102
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@@ -81,8 +81,35 @@ param set-default MAV_TYPE 22
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param set-default SENS_DPRES_OFF 0.001
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#
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# # gazebo model:
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# # https://github.com/PX4/PX4-gazebo-models/blob/main/models/standard_vtol/model.sdf
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# # notes about gazebo models:
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# # https://github.com/mvernacc/gazebo_motor_model_docs/blob/master/notes.pdf
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#
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# # max thrust = maxRotVelocity**2 * motorConstant
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# param set SIH_T_MAX 45
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#
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# # max torque = ??
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# param set SIH_Q_MAX 0.0165
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#
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# # = base_link mass (rest irrelevant)
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# param set SIH_MASS 5
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#
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# param set SIH_IXX 0.4777
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# param set SIH_IYY 0.3417
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# param set SIH_IZZ 0.8110
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# param set SIH_IXZ 0
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#
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# param set SIH_KDV 0.2
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#
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# param set SIH_T_MAX 6.5
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# param set SIH_MASS 0.65
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param set SIH_T_MAX 2.0
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param set SIH_Q_MAX 0.0165
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param set SIH_MASS 0.2
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# IXX and IZZ are inverted from the thesis as the body frame is pitched by 90 deg
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param set SIH_IXX 0.00354
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