mirror of https://github.com/ArduPilot/ardupilot
407 lines
17 KiB
C++
407 lines
17 KiB
C++
#include "AC_CustomControl_PID.h"
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#include "AC_AttitudeControl/AC_AttitudeControl_Multi.h"
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#if CUSTOMCONTROL_PID_ENABLED
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// table of user settable parameters
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const AP_Param::GroupInfo AC_CustomControl_PID::var_info[] = {
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// @Param: ANG_RLL_P
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// @DisplayName: Roll axis angle controller P gain
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// @Description: Roll axis angle controller P gain. Converts the error between the desired roll angle and actual angle to a desired roll rate
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// @Range: 3.000 12.000
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// @Range{Sub}: 0.0 12.000
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// @User: Standard
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AP_SUBGROUPINFO(_p_angle_roll2, "ANG_RLL_", 1, AC_CustomControl_PID, AC_P),
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// @Param: ANG_PIT_P
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// @DisplayName: Pitch axis angle controller P gain
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// @Description: Pitch axis angle controller P gain. Converts the error between the desired pitch angle and actual angle to a desired pitch rate
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// @Range: 3.000 12.000
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// @Range{Sub}: 0.0 12.000
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// @User: Standard
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AP_SUBGROUPINFO(_p_angle_pitch2, "ANG_PIT_", 2, AC_CustomControl_PID, AC_P),
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// @Param: ANG_YAW_P
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// @DisplayName: Yaw axis angle controller P gain
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// @Description: Yaw axis angle controller P gain. Converts the error between the desired yaw angle and actual angle to a desired yaw rate
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// @Range: 3.000 12.000
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// @Range{Sub}: 0.0 6.000
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// @User: Standard
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AP_SUBGROUPINFO(_p_angle_yaw2, "ANG_YAW_", 3, AC_CustomControl_PID, AC_P),
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// @Param: RAT_RLL_P
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// @DisplayName: Roll axis rate controller P gain
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// @Description: Roll axis rate controller P gain. Corrects in proportion to the difference between the desired roll rate vs actual roll rate
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// @Range: 0.01 0.5
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// @Increment: 0.005
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// @User: Standard
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// @Param: RAT_RLL_I
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// @DisplayName: Roll axis rate controller I gain
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// @Description: Roll axis rate controller I gain. Corrects long-term difference in desired roll rate vs actual roll rate
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// @Range: 0.01 2.0
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// @Increment: 0.01
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// @User: Standard
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// @Param: RAT_RLL_IMAX
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// @DisplayName: Roll axis rate controller I gain maximum
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// @Description: Roll axis rate controller I gain maximum. Constrains the maximum that the I term will output
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// @Range: 0 1
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// @Increment: 0.01
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// @User: Standard
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// @Param: RAT_RLL_D
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// @DisplayName: Roll axis rate controller D gain
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// @Description: Roll axis rate controller D gain. Compensates for short-term change in desired roll rate vs actual roll rate
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// @Range: 0.0 0.05
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// @Increment: 0.001
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// @User: Standard
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// @Param: RAT_RLL_FF
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// @DisplayName: Roll axis rate controller feed forward
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// @Description: Roll axis rate controller feed forward
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// @Range: 0 0.5
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// @Increment: 0.001
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// @User: Standard
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// @Param: RAT_RLL_FLTT
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// @DisplayName: Roll axis rate controller target frequency in Hz
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// @Description: Roll axis rate controller target frequency in Hz
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// @Range: 5 100
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// @Increment: 1
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// @Units: Hz
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// @User: Standard
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// @Param: RAT_RLL_FLTE
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// @DisplayName: Roll axis rate controller error frequency in Hz
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// @Description: Roll axis rate controller error frequency in Hz
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// @Range: 0 100
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// @Increment: 1
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// @Units: Hz
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// @User: Standard
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// @Param: RAT_RLL_FLTD
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// @DisplayName: Roll axis rate controller derivative frequency in Hz
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// @Description: Roll axis rate controller derivative frequency in Hz
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// @Range: 5 100
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// @Increment: 1
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// @Units: Hz
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// @User: Standard
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// @Param: RAT_RLL_SMAX
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// @DisplayName: Roll slew rate limit
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// @Description: Sets an upper limit on the slew rate produced by the combined P and D gains. If the amplitude of the control action produced by the rate feedback exceeds this value, then the D+P gain is reduced to respect the limit. This limits the amplitude of high frequency oscillations caused by an excessive gain. The limit should be set to no more than 25% of the actuators maximum slew rate to allow for load effects. Note: The gain will not be reduced to less than 10% of the nominal value. A value of zero will disable this feature.
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// @Range: 0 200
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// @Increment: 0.5
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// @User: Advanced
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// @Param: RAT_RLL_PDMX
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// @DisplayName: Roll axis rate controller PD sum maximum
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// @Description: Roll axis rate controller PD sum maximum. The maximum/minimum value that the sum of the P and D term can output
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// @Range: 0 1
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// @Increment: 0.01
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// @User: Advanced
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// @Param: RAT_RLL_D_FF
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// @DisplayName: Roll Derivative FeedForward Gain
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// @Description: FF D Gain which produces an output that is proportional to the rate of change of the target
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// @Range: 0 0.02
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// @Increment: 0.0001
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// @User: Advanced
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// @Param: RAT_RLL_NTF
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// @DisplayName: Roll Target notch filter index
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// @Description: Roll Target notch filter index
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// @Range: 1 8
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// @User: Advanced
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// @Param: RAT_RLL_NEF
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// @DisplayName: Roll Error notch filter index
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// @Description: Roll Error notch filter index
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// @Range: 1 8
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// @User: Advanced
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AP_SUBGROUPINFO(_pid_atti_rate_roll, "RAT_RLL_", 4, AC_CustomControl_PID, AC_PID),
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// @Param: RAT_PIT_P
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// @DisplayName: Pitch axis rate controller P gain
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// @Description: Pitch axis rate controller P gain. Corrects in proportion to the difference between the desired pitch rate vs actual pitch rate
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// @Range: 0.01 0.50
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// @Increment: 0.005
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// @User: Standard
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// @Param: RAT_PIT_I
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// @DisplayName: Pitch axis rate controller I gain
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// @Description: Pitch axis rate controller I gain. Corrects long-term difference in desired pitch rate vs actual pitch rate
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// @Range: 0.01 2.0
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// @Increment: 0.01
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// @User: Standard
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// @Param: RAT_PIT_IMAX
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// @DisplayName: Pitch axis rate controller I gain maximum
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// @Description: Pitch axis rate controller I gain maximum. Constrains the maximum that the I term will output
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// @Range: 0 1
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// @Increment: 0.01
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// @User: Standard
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// @Param: RAT_PIT_D
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// @DisplayName: Pitch axis rate controller D gain
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// @Description: Pitch axis rate controller D gain. Compensates for short-term change in desired pitch rate vs actual pitch rate
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// @Range: 0.0 0.05
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// @Increment: 0.001
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// @User: Standard
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// @Param: RAT_PIT_FF
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// @DisplayName: Pitch axis rate controller feed forward
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// @Description: Pitch axis rate controller feed forward
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// @Range: 0 0.5
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// @Increment: 0.001
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// @User: Standard
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// @Param: RAT_PIT_FLTT
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// @DisplayName: Pitch axis rate controller target frequency in Hz
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// @Description: Pitch axis rate controller target frequency in Hz
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// @Range: 5 100
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// @Increment: 1
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// @Units: Hz
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// @User: Standard
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// @Param: RAT_PIT_FLTE
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// @DisplayName: Pitch axis rate controller error frequency in Hz
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// @Description: Pitch axis rate controller error frequency in Hz
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// @Range: 0 100
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// @Increment: 1
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// @Units: Hz
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// @User: Standard
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// @Param: RAT_PIT_FLTD
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// @DisplayName: Pitch axis rate controller derivative frequency in Hz
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// @Description: Pitch axis rate controller derivative frequency in Hz
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// @Range: 5 100
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// @Increment: 1
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// @Units: Hz
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// @User: Standard
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// @Param: RAT_PIT_SMAX
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// @DisplayName: Pitch slew rate limit
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// @Description: Sets an upper limit on the slew rate produced by the combined P and D gains. If the amplitude of the control action produced by the rate feedback exceeds this value, then the D+P gain is reduced to respect the limit. This limits the amplitude of high frequency oscillations caused by an excessive gain. The limit should be set to no more than 25% of the actuators maximum slew rate to allow for load effects. Note: The gain will not be reduced to less than 10% of the nominal value. A value of zero will disable this feature.
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// @Range: 0 200
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// @Increment: 0.5
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// @User: Advanced
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// @Param: RAT_PIT_PDMX
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// @DisplayName: Pitch axis rate controller PD sum maximum
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// @Description: Pitch axis rate controller PD sum maximum. The maximum/minimum value that the sum of the P and D term can output
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// @Range: 0 1
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// @Increment: 0.01
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// @User: Advanced
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// @Param: RAT_PIT_D_FF
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// @DisplayName: Pitch Derivative FeedForward Gain
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// @Description: FF D Gain which produces an output that is proportional to the rate of change of the target
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// @Range: 0 0.02
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// @Increment: 0.0001
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// @User: Advanced
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// @Param: RAT_PIT_NTF
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// @DisplayName: Pitch Target notch filter index
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// @Description: Pitch Target notch filter index
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// @Range: 1 8
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// @User: Advanced
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// @Param: RAT_PIT_NEF
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// @DisplayName: Pitch Error notch filter index
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// @Description: Pitch Error notch filter index
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// @Range: 1 8
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// @User: Advanced
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AP_SUBGROUPINFO(_pid_atti_rate_pitch, "RAT_PIT_", 5, AC_CustomControl_PID, AC_PID),
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// @Param: RAT_YAW_P
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// @DisplayName: Yaw axis rate controller P gain
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// @Description: Yaw axis rate controller P gain. Corrects in proportion to the difference between the desired yaw rate vs actual yaw rate
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// @Range: 0.10 2.50
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// @Increment: 0.005
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// @User: Standard
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// @Param: RAT_YAW_I
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// @DisplayName: Yaw axis rate controller I gain
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// @Description: Yaw axis rate controller I gain. Corrects long-term difference in desired yaw rate vs actual yaw rate
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// @Range: 0.010 1.0
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// @Increment: 0.01
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// @User: Standard
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// @Param: RAT_YAW_IMAX
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// @DisplayName: Yaw axis rate controller I gain maximum
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// @Description: Yaw axis rate controller I gain maximum. Constrains the maximum that the I term will output
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// @Range: 0 1
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// @Increment: 0.01
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// @User: Standard
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// @Param: RAT_YAW_D
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// @DisplayName: Yaw axis rate controller D gain
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// @Description: Yaw axis rate controller D gain. Compensates for short-term change in desired yaw rate vs actual yaw rate
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// @Range: 0.000 0.02
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// @Increment: 0.001
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// @User: Standard
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// @Param: RAT_YAW_FF
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// @DisplayName: Yaw axis rate controller feed forward
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// @Description: Yaw axis rate controller feed forward
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// @Range: 0 0.5
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// @Increment: 0.001
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// @User: Standard
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// @Param: RAT_YAW_FLTT
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// @DisplayName: Yaw axis rate controller target frequency in Hz
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// @Description: Yaw axis rate controller target frequency in Hz
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// @Range: 1 50
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// @Increment: 1
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// @Units: Hz
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// @User: Standard
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// @Param: RAT_YAW_FLTE
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// @DisplayName: Yaw axis rate controller error frequency in Hz
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// @Description: Yaw axis rate controller error frequency in Hz
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// @Range: 0 20
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// @Increment: 1
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// @Units: Hz
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// @User: Standard
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// @Param: RAT_YAW_FLTD
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// @DisplayName: Yaw axis rate controller derivative frequency in Hz
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// @Description: Yaw axis rate controller derivative frequency in Hz
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// @Range: 5 50
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// @Increment: 1
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// @Units: Hz
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// @User: Standard
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// @Param: RAT_YAW_SMAX
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// @DisplayName: Yaw slew rate limit
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// @Description: Sets an upper limit on the slew rate produced by the combined P and D gains. If the amplitude of the control action produced by the rate feedback exceeds this value, then the D+P gain is reduced to respect the limit. This limits the amplitude of high frequency oscillations caused by an excessive gain. The limit should be set to no more than 25% of the actuators maximum slew rate to allow for load effects. Note: The gain will not be reduced to less than 10% of the nominal value. A value of zero will disable this feature.
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// @Range: 0 200
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// @Increment: 0.5
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// @User: Advanced
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// @Param: RAT_YAW_PDMX
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// @DisplayName: Yaw axis rate controller PD sum maximum
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// @Description: Yaw axis rate controller PD sum maximum. The maximum/minimum value that the sum of the P and D term can output
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// @Range: 0 1
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// @Increment: 0.01
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// @User: Advanced
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// @Param: RAT_YAW_D_FF
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// @DisplayName: Yaw Derivative FeedForward Gain
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// @Description: FF D Gain which produces an output that is proportional to the rate of change of the target
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// @Range: 0 0.02
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// @Increment: 0.0001
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// @User: Advanced
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// @Param: RAT_YAW_NTF
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// @DisplayName: Yaw Target notch filter index
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// @Description: Yaw Target notch filter index
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// @Range: 1 8
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// @User: Advanced
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// @Param: RAT_YAW_NEF
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// @DisplayName: Yaw Error notch filter index
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// @Description: Yaw Error notch filter index
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// @Range: 1 8
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// @User: Advanced
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AP_SUBGROUPINFO(_pid_atti_rate_yaw, "RAT_YAW_", 6, AC_CustomControl_PID, AC_PID),
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AP_GROUPEND
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};
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AC_CustomControl_PID::AC_CustomControl_PID(AC_CustomControl& frontend, AP_AHRS_View*& ahrs, AC_AttitudeControl*& att_control, AP_MotorsMulticopter*& motors, float dt) :
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AC_CustomControl_Backend(frontend, ahrs, att_control, motors, dt),
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_p_angle_roll2(AC_ATTITUDE_CONTROL_ANGLE_P * 0.90f),
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_p_angle_pitch2(AC_ATTITUDE_CONTROL_ANGLE_P * 0.90f),
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_p_angle_yaw2(AC_ATTITUDE_CONTROL_ANGLE_P * 0.90f),
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_pid_atti_rate_roll(AC_ATC_MULTI_RATE_RP_P * 0.90f, AC_ATC_MULTI_RATE_RP_I * 0.90f, AC_ATC_MULTI_RATE_RP_D * 0.90f, 0.0f, AC_ATC_MULTI_RATE_RP_IMAX * 0.90f, AC_ATC_MULTI_RATE_RPY_FILT_HZ * 0.90f, 0.0f, AC_ATC_MULTI_RATE_RPY_FILT_HZ * 0.90f),
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_pid_atti_rate_pitch(AC_ATC_MULTI_RATE_RP_P * 0.90f, AC_ATC_MULTI_RATE_RP_I * 0.90f, AC_ATC_MULTI_RATE_RP_D * 0.90f, 0.0f, AC_ATC_MULTI_RATE_RP_IMAX * 0.90f, AC_ATC_MULTI_RATE_RPY_FILT_HZ * 0.90f, 0.0f, AC_ATC_MULTI_RATE_RPY_FILT_HZ * 0.90f),
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_pid_atti_rate_yaw(AC_ATC_MULTI_RATE_YAW_P * 0.90f, AC_ATC_MULTI_RATE_YAW_I * 0.90f, AC_ATC_MULTI_RATE_YAW_D * 0.90f, 0.0f, AC_ATC_MULTI_RATE_YAW_IMAX * 0.90f, AC_ATC_MULTI_RATE_RPY_FILT_HZ * 0.90f, AC_ATC_MULTI_RATE_YAW_FILT_HZ * 0.90f, 0.0f)
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{
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_dt = dt;
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AP_Param::setup_object_defaults(this, var_info);
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}
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Vector3f AC_CustomControl_PID::update()
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{
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// reset controller based on spool state
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switch (_motors->get_spool_state()) {
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case AP_Motors::SpoolState::SHUT_DOWN:
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case AP_Motors::SpoolState::GROUND_IDLE:
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// We are still at the ground. Reset custom controller to avoid
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// build up, ex: integrator
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reset();
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break;
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case AP_Motors::SpoolState::THROTTLE_UNLIMITED:
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case AP_Motors::SpoolState::SPOOLING_UP:
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case AP_Motors::SpoolState::SPOOLING_DOWN:
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// we are off the ground
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break;
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}
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// run custom controller after here
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Quaternion attitude_body, attitude_target;
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_ahrs->get_quat_body_to_ned(attitude_body);
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attitude_target = _att_control->get_attitude_target_quat();
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// This vector represents the angular error to rotate the thrust vector using x and y and heading using z
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Vector3f attitude_error;
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float _thrust_angle, _thrust_error_angle;
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_att_control->thrust_heading_rotation_angles(attitude_target, attitude_body, attitude_error, _thrust_angle, _thrust_error_angle);
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// recalculate ang vel feedforward from attitude target model
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// rotation from the target frame to the body frame
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Quaternion rotation_target_to_body = attitude_body.inverse() * attitude_target;
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// target angle velocity vector in the body frame
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Vector3f ang_vel_body_feedforward = rotation_target_to_body * _att_control->get_attitude_target_ang_vel();
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// run attitude controller
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Vector3f target_rate;
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target_rate[0] = _p_angle_roll2.kP() * attitude_error.x + ang_vel_body_feedforward[0];
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target_rate[1] = _p_angle_pitch2.kP() * attitude_error.y + ang_vel_body_feedforward[1];
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target_rate[2] = _p_angle_yaw2.kP() * attitude_error.z + ang_vel_body_feedforward[2];
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// run rate controller
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Vector3f gyro_latest = _ahrs->get_gyro_latest();
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Vector3f motor_out;
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motor_out.x = _pid_atti_rate_roll.update_all(target_rate[0], gyro_latest[0], _dt, false);
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motor_out.y = _pid_atti_rate_pitch.update_all(target_rate[1], gyro_latest[1], _dt, false);
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motor_out.z = _pid_atti_rate_yaw.update_all(target_rate[2], gyro_latest[2], _dt, false);
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return motor_out;
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}
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// This example uses exact same controller architecture as ArduCopter attitude controller without all the safe guard against saturation.
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// The gains are scaled 0.9 times to better detect switch over response.
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// Note that integrator are not reset correctly as it is done in reset_main_att_controller inside AC_CustomControl.cpp
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// This is done intentionally to demonstrate switch over performance of two exact controller with different reset handling.
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void AC_CustomControl_PID::reset(void)
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{
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_pid_atti_rate_roll.reset_I();
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_pid_atti_rate_pitch.reset_I();
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_pid_atti_rate_yaw.reset_I();
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_pid_atti_rate_roll.reset_filter();
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_pid_atti_rate_pitch.reset_filter();
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_pid_atti_rate_yaw.reset_filter();
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}
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void AC_CustomControl_PID::set_notch_sample_rate(float sample_rate)
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{
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#if AP_FILTER_ENABLED
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_pid_atti_rate_roll.set_notch_sample_rate(sample_rate);
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_pid_atti_rate_pitch.set_notch_sample_rate(sample_rate);
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_pid_atti_rate_yaw.set_notch_sample_rate(sample_rate);
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#endif
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}
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#endif
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