AP_MotorsHeli: Create SV_MAN=5=Oscillate servo setup mode.

This commit is contained in:
Robert Lefebvre 2015-10-21 16:00:36 -04:00 committed by Randy Mackay
parent 4443ca9602
commit eeb544d098
4 changed files with 64 additions and 0 deletions

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@ -277,6 +277,10 @@ void AP_MotorsHeli::output_disarmed()
_throttle_control_input = 0;
_yaw_control_input = -4500;
break;
case SERVO_CONTROL_MODE_MANUAL_OSCILLATE:
// use servo_test function from child classes
servo_test();
break;
default:
// no manual override
break;

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@ -153,6 +153,10 @@ public:
// reset_radio_passthrough used to reset all radio inputs to center
void reset_radio_passthrough();
// servo_test - move servos through full range of movement
// to be overloaded by child classes, different vehicle types would have different movement patterns
virtual void servo_test() = 0;
// output - sends commands to the motors
void output();
@ -163,6 +167,7 @@ public:
SERVO_CONTROL_MODE_MANUAL_MAX,
SERVO_CONTROL_MODE_MANUAL_CENTER,
SERVO_CONTROL_MODE_MANUAL_MIN,
SERVO_CONTROL_MODE_MANUAL_OSCILLATE,
};
// supports_yaw_passthrough

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@ -478,3 +478,55 @@ void AP_MotorsHeli_Single::write_aux(int16_t servo_out)
_servo_aux.calc_pwm();
hal.rcout->write(AP_MOTORS_HELI_SINGLE_AUX, _servo_aux.radio_out);
}
// servo_test - move servos through full range of movement
void AP_MotorsHeli_Single::servo_test()
{
static float oscillate_angle = 0.0f;
static float servo_test_cycle_time = 0.0f;
static float collective_test = 0.0f;
static float roll_test = 0.0f;
static float pitch_test = 0.0f;
static float yaw_test = 0.0f;
servo_test_cycle_time += 1.0f / _loop_rate;
if ((servo_test_cycle_time >= 0.0f && servo_test_cycle_time < 0.5f)|| // Tilt swash back
(servo_test_cycle_time >= 6.0f && servo_test_cycle_time < 6.5f)){
pitch_test += (4500 / (_loop_rate/2));
oscillate_angle += 8 * M_PI_F / _loop_rate;
yaw_test = 2250 * sinf(oscillate_angle);
} else if ((servo_test_cycle_time >= 0.5f && servo_test_cycle_time < 4.5f)|| // Roll swash around
(servo_test_cycle_time >= 6.5f && servo_test_cycle_time < 10.5f)){
oscillate_angle += M_PI_F / (2 * _loop_rate);
roll_test = 4500 * sinf(oscillate_angle);
pitch_test = 4500 * cosf(oscillate_angle);
yaw_test = 4500 * sinf(oscillate_angle);
} else if ((servo_test_cycle_time >= 4.5f && servo_test_cycle_time < 5.0f)|| // Return swash to level
(servo_test_cycle_time >= 10.5f && servo_test_cycle_time < 11.0f)){
pitch_test -= (4500 / (_loop_rate/2));
oscillate_angle += 8 * M_PI_F / _loop_rate;
yaw_test = 2250 * sinf(oscillate_angle);
} else if (servo_test_cycle_time >= 5.0f && servo_test_cycle_time < 6.0f){ // Raise swash to top
collective_test += (1000 / _loop_rate);
oscillate_angle += 2 * M_PI_F / _loop_rate;
yaw_test = 4500 * sinf(oscillate_angle);
} else if (servo_test_cycle_time >= 11.0f && servo_test_cycle_time < 12.0f){ // Lower swash to bottom
collective_test -= (1000 / _loop_rate);
oscillate_angle += 2 * M_PI_F / _loop_rate;
yaw_test = 4500 * sinf(oscillate_angle);
} else { // reset cycle
servo_test_cycle_time = 0.0f;
oscillate_angle = 0.0f;
collective_test = 0.0f;
roll_test = 0.0f;
pitch_test = 0.0f;
yaw_test = 0.0f;
}
// over-ride servo commands to move servos through defined ranges
_throttle_control_input = collective_test;
_roll_control_input = roll_test;
_pitch_control_input = pitch_test;
_yaw_control_input = yaw_test;
}

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@ -121,6 +121,9 @@ public:
void set_acro_tail(bool set) { _acro_tail = set; }
// servo_test - move servos through full range of movement
void servo_test();
// var_info
static const struct AP_Param::GroupInfo var_info[];