Plane: support motor_test for quadplanes

This commit is contained in:
Andrew Tridgell 2016-03-13 10:05:10 +11:00
parent d644474817
commit 89970e4eaa
4 changed files with 149 additions and 1 deletions

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@ -1539,6 +1539,14 @@ void GCS_MAVLINK::handleMessage(mavlink_message_t* msg)
break;
#endif
case MAV_CMD_DO_MOTOR_TEST:
// param1 : motor sequence number (a number from 1 to max number of motors on the vehicle)
// param2 : throttle type (0=throttle percentage, 1=PWM, 2=pilot throttle channel pass-through. See MOTOR_TEST_THROTTLE_TYPE enum)
// param3 : throttle (range depends upon param2)
// param4 : timeout (in seconds)
result = plane.quadplane.mavlink_motor_test_start(chan, (uint8_t)packet.param1, (uint8_t)packet.param2, (uint16_t)packet.param3, packet.param4);
break;
case MAV_CMD_DO_VTOL_TRANSITION:
result = plane.quadplane.handle_do_vtol_transition(packet);
break;

118
ArduPlane/motor_test.cpp Normal file
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@ -0,0 +1,118 @@
// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
#include "Plane.h"
/*
mavlink motor test - implements the MAV_CMD_DO_MOTOR_TEST mavlink
command so that the quadplane pilot can test an
individual motor to ensure proper wiring, rotation.
*/
// motor test definitions
#define MOTOR_TEST_PWM_MIN 800 // min pwm value accepted by the test
#define MOTOR_TEST_PWM_MAX 2200 // max pwm value accepted by the test
#define MOTOR_TEST_TIMEOUT_MS_MAX 30000 // max timeout is 30 seconds
// motor_test_output - checks for timeout and sends updates to motors objects
void QuadPlane::motor_test_output()
{
// exit immediately if the motor test is not running
if (!motor_test.running) {
return;
}
// check for test timeout
if ((AP_HAL::millis() - motor_test.start_ms) >= motor_test.timeout_ms) {
// stop motor test
motor_test_stop();
return;
}
int16_t pwm = 0; // pwm that will be output to the motors
// calculate pwm based on throttle type
switch (motor_test.throttle_type) {
case MOTOR_TEST_THROTTLE_PERCENT:
// sanity check motor_test.throttle value
if (motor_test.throttle_value <= 100) {
pwm = plane.channel_throttle->radio_min + (plane.channel_throttle->radio_max - plane.channel_throttle->radio_min) * (float)motor_test.throttle_value/100.0f;
}
break;
case MOTOR_TEST_THROTTLE_PWM:
pwm = motor_test.throttle_value;
break;
case MOTOR_TEST_THROTTLE_PILOT:
pwm = plane.channel_throttle->radio_in;
break;
default:
motor_test_stop();
return;
}
// sanity check throttle values
if (pwm >= MOTOR_TEST_PWM_MIN && pwm <= MOTOR_TEST_PWM_MAX ) {
// turn on motor to specified pwm vlaue
motors->output_test(motor_test.seq, pwm);
} else {
motor_test_stop();
}
}
// mavlink_motor_test_start - start motor test - spin a single motor at a specified pwm
// returns MAV_RESULT_ACCEPTED on success, MAV_RESULT_FAILED on failure
uint8_t QuadPlane::mavlink_motor_test_start(mavlink_channel_t chan, uint8_t motor_seq, uint8_t throttle_type,
uint16_t throttle_value, float timeout_sec)
{
if (motors->armed()) {
plane.gcs_send_text(MAV_SEVERITY_INFO, "Must be disarmed for motor test");
return MAV_RESULT_FAILED;
}
// if test has not started try to start it
if (!motor_test.running) {
// start test
motor_test.running = true;
// enable and arm motors
set_armed(true);
// turn on notify leds
AP_Notify::flags.esc_calibration = true;
}
// set timeout
motor_test.start_ms = AP_HAL::millis();
motor_test.timeout_ms = MIN(timeout_sec * 1000, MOTOR_TEST_TIMEOUT_MS_MAX);
// store required output
motor_test.seq = motor_seq;
motor_test.throttle_type = throttle_type;
motor_test.throttle_value = throttle_value;
// return success
return MAV_RESULT_ACCEPTED;
}
// motor_test_stop - stops the motor test
void QuadPlane::motor_test_stop()
{
// exit immediately if the test is not running
if (!motor_test.running) {
return;
}
// flag test is complete
motor_test.running = false;
// disarm motors
set_armed(false);
// reset timeout
motor_test.start_ms = 0;
motor_test.timeout_ms = 0;
// turn off notify leds
AP_Notify::flags.esc_calibration = false;
}

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@ -335,7 +335,7 @@ const AP_Param::GroupInfo QuadPlane::var_info[] = {
// @Param: FRAME_CLASS
// @DisplayName: Frame Class
// @Description: Controls major frame class for multicopter component
// @Values: 0:Quad, 1:Hexa, 2:Octa
// @Values: 0:Quad, 1:Hexa, 2:Octa, 3:OctaQuad
// @User: Standard
AP_GROUPINFO("FRAME_CLASS", 30, QuadPlane, frame_class, 0),
@ -875,6 +875,11 @@ void QuadPlane::update(void)
return;
}
if (motor_test.running) {
motor_test_output();
return;
}
if (!in_vtol_mode()) {
update_transition();
} else {

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@ -200,5 +200,22 @@ private:
FRAME_CLASS_QUAD=0,
FRAME_CLASS_HEXA=1,
FRAME_CLASS_OCTA=2,
FRAME_CLASS_OCTAQUAD=3,
};
struct {
bool running;
uint32_t start_ms; // system time the motor test began
uint32_t timeout_ms = 0; // test will timeout this many milliseconds after the motor_test_start_ms
uint8_t seq = 0; // motor sequence number of motor being tested
uint8_t throttle_type = 0; // motor throttle type (0=throttle percentage, 1=PWM, 2=pilot throttle channel pass-through)
uint16_t throttle_value = 0; // throttle to be sent to motor, value depends upon it's type
} motor_test;
public:
void motor_test_output();
uint8_t mavlink_motor_test_start(mavlink_channel_t chan, uint8_t motor_seq, uint8_t throttle_type,
uint16_t throttle_value, float timeout_sec);
private:
void motor_test_stop();
};