4 changed files with 149 additions and 1 deletions
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// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
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#include "Plane.h" |
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/*
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mavlink motor test - implements the MAV_CMD_DO_MOTOR_TEST mavlink |
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command so that the quadplane pilot can test an |
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individual motor to ensure proper wiring, rotation. |
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*/ |
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// motor test definitions
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#define MOTOR_TEST_PWM_MIN 800 // min pwm value accepted by the test
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#define MOTOR_TEST_PWM_MAX 2200 // max pwm value accepted by the test
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#define MOTOR_TEST_TIMEOUT_MS_MAX 30000 // max timeout is 30 seconds
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// motor_test_output - checks for timeout and sends updates to motors objects
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void QuadPlane::motor_test_output() |
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{ |
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// exit immediately if the motor test is not running
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if (!motor_test.running) { |
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return; |
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} |
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// check for test timeout
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if ((AP_HAL::millis() - motor_test.start_ms) >= motor_test.timeout_ms) { |
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// stop motor test
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motor_test_stop(); |
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return; |
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} |
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int16_t pwm = 0; // pwm that will be output to the motors
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// calculate pwm based on throttle type
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switch (motor_test.throttle_type) { |
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case MOTOR_TEST_THROTTLE_PERCENT: |
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// sanity check motor_test.throttle value
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if (motor_test.throttle_value <= 100) { |
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pwm = plane.channel_throttle->radio_min + (plane.channel_throttle->radio_max - plane.channel_throttle->radio_min) * (float)motor_test.throttle_value/100.0f; |
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} |
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break; |
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case MOTOR_TEST_THROTTLE_PWM: |
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pwm = motor_test.throttle_value; |
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break; |
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case MOTOR_TEST_THROTTLE_PILOT: |
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pwm = plane.channel_throttle->radio_in; |
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break; |
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default: |
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motor_test_stop(); |
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return; |
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} |
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// sanity check throttle values
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if (pwm >= MOTOR_TEST_PWM_MIN && pwm <= MOTOR_TEST_PWM_MAX ) { |
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// turn on motor to specified pwm vlaue
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motors->output_test(motor_test.seq, pwm); |
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} else { |
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motor_test_stop(); |
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} |
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} |
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// mavlink_motor_test_start - start motor test - spin a single motor at a specified pwm
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// returns MAV_RESULT_ACCEPTED on success, MAV_RESULT_FAILED on failure
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uint8_t QuadPlane::mavlink_motor_test_start(mavlink_channel_t chan, uint8_t motor_seq, uint8_t throttle_type, |
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uint16_t throttle_value, float timeout_sec) |
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{ |
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if (motors->armed()) { |
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plane.gcs_send_text(MAV_SEVERITY_INFO, "Must be disarmed for motor test"); |
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return MAV_RESULT_FAILED; |
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} |
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// if test has not started try to start it
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if (!motor_test.running) { |
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// start test
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motor_test.running = true; |
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// enable and arm motors
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set_armed(true); |
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// turn on notify leds
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AP_Notify::flags.esc_calibration = true; |
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} |
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// set timeout
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motor_test.start_ms = AP_HAL::millis(); |
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motor_test.timeout_ms = MIN(timeout_sec * 1000, MOTOR_TEST_TIMEOUT_MS_MAX); |
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// store required output
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motor_test.seq = motor_seq; |
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motor_test.throttle_type = throttle_type; |
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motor_test.throttle_value = throttle_value; |
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// return success
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return MAV_RESULT_ACCEPTED; |
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} |
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// motor_test_stop - stops the motor test
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void QuadPlane::motor_test_stop() |
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{ |
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// exit immediately if the test is not running
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if (!motor_test.running) { |
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return; |
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} |
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// flag test is complete
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motor_test.running = false; |
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// disarm motors
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set_armed(false); |
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// reset timeout
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motor_test.start_ms = 0; |
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motor_test.timeout_ms = 0; |
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// turn off notify leds
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AP_Notify::flags.esc_calibration = false; |
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} |
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