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https://github.com/ArduPilot/ardupilot
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AP_Motors: added reached_limit method which returns bit mask indicating which control inputs could not be achieved
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@ -50,6 +50,12 @@
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#define THROTTLE_CURVE_MID_THRUST 52 // throttle which produces 1/2 the maximum thrust. expressed as a percentage of the full throttle range (i.e 0 ~ 100)
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#define THROTTLE_CURVE_MAX_THRUST 93 // throttle which produces the maximum thrust. expressed as a percentage of the full throttle range (i.e 0 ~ 100)
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// bit mask for recording which limits we have reached when outputting to motors
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#define AP_MOTOR_NO_LIMITS_REACHED 0x00
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#define AP_MOTOR_ROLLPITCH_LIMIT 0x01
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#define AP_MOTOR_YAW_LIMIT 0x02
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#define AP_MOTOR_THROTTLE_LIMIT 0x04
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/// @class AP_Motors
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class AP_Motors {
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public:
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@ -120,6 +126,11 @@ public:
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virtual void output_min() {
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};
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// reached_limits - return whether we hit the limits of the motors
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virtual uint8_t reached_limit( uint8_t which_limit = 0x00 ) {
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return _reached_limit & which_limit;
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}
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// get basic information about the platform
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virtual uint8_t get_num_motors() {
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return 0;
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@ -169,6 +180,7 @@ protected:
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AP_Int8 _throttle_curve_enabled; // enable throttle curve
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AP_Int8 _throttle_curve_mid; // throttle which produces 1/2 the maximum thrust. expressed as a percentage (i.e. 0 ~ 100 ) of the full throttle range
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AP_Int8 _throttle_curve_max; // throttle which produces the maximum thrust. expressed as a percentage (i.e. 0 ~ 100 ) of the full throttle range
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uint8_t _reached_limit; // bit mask to record which motor limits we hit (if any) during most recent output. Used to provide feedback to attitude controllers
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};
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#endif // AP_MOTORS
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@ -109,18 +109,36 @@ void AP_MotorsMatrix::output_armed()
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int16_t motor_adjustment = 0;
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int16_t yaw_to_execute = 0;
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// initialize reached_limit flag
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_reached_limit = AP_MOTOR_NO_LIMITS_REACHED;
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// Throttle is 0 to 1000 only
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_rc_throttle->servo_out = constrain(_rc_throttle->servo_out, 0, _max_throttle);
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if(_rc_throttle->servo_out > 0)
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out_min = _rc_throttle->radio_min + _min_throttle;
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// capture desired roll, pitch, yaw and throttle from receiver
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_rc_roll->calc_pwm();
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_rc_pitch->calc_pwm();
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_rc_throttle->calc_pwm();
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_rc_yaw->calc_pwm();
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// if we are not sending a throttle output, we cut the motors
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if(_rc_throttle->servo_out == 0) {
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for( i=0; i<AP_MOTORS_MAX_NUM_MOTORS; i++ ) {
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if( motor_enabled[i] ) {
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motor_out[i] = _rc_throttle->radio_min;
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}
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}
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// if we have any roll, pitch or yaw input then it's breaching the limit
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if( _rc_roll->pwm_out != 0 || _rc_pitch->pwm_out != 0 ) {
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_reached_limit |= AP_MOTOR_ROLLPITCH_LIMIT;
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}
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if( _rc_yaw->pwm_out != 0 ) {
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_reached_limit |= AP_MOTOR_YAW_LIMIT;
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}
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} else { // non-zero throttle
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out_min = _rc_throttle->radio_min + _min_throttle;
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// initialise rc_yaw_contrained_pwm that we will certainly output and rc_yaw_excess that we will do on best-efforts basis.
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// Note: these calculations and many others below depend upon _yaw_factors always being 0, -1 or 1.
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if( _rc_yaw->pwm_out < -AP_MOTORS_MATRIX_YAW_LOWER_LIMIT_PWM ) {
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@ -180,6 +198,9 @@ void AP_MotorsMatrix::output_armed()
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motor_out[i] += motor_adjustment;
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}
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}
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// we haven't even been able to apply roll, pitch and minimal yaw without adjusting throttle so mark all limits as breached
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_reached_limit |= AP_MOTOR_ROLLPITCH_LIMIT | AP_MOTOR_YAW_LIMIT | AP_MOTOR_THROTTLE_LIMIT;
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}
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// if we didn't give all the yaw requested, calculate how much additional yaw we can add
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@ -226,6 +247,10 @@ void AP_MotorsMatrix::output_armed()
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}
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}
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}
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// mark yaw limit reached if we didn't get everything we asked for
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if( yaw_to_execute != rc_yaw_excess ) {
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_reached_limit |= AP_MOTOR_YAW_LIMIT;
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}
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}
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// adjust for throttle curve
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@ -243,17 +268,7 @@ void AP_MotorsMatrix::output_armed()
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motor_out[i] = constrain(motor_out[i], out_min, out_max);
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}
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}
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#if CUT_MOTORS == ENABLED
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// if we are not sending a throttle output, we cut the motors
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if(_rc_throttle->servo_out == 0) {
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for( i=0; i<AP_MOTORS_MAX_NUM_MOTORS; i++ ) {
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if( motor_enabled[i] ) {
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motor_out[i] = _rc_throttle->radio_min;
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}
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}
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}
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#endif
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// send output to each motor
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for( i=0; i<AP_MOTORS_MAX_NUM_MOTORS; i++ ) {
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