aboutsummaryrefslogtreecommitdiff
path: root/src/modules/commander/airspeed_calibration.c
blob: feaf11aee7431886a9bf670045f58096878b10b6 (plain) (blame)
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
82
83
84
85
86
87
88
89
90
91
92
93
94
95
96
97
98
99
100
101
102
103
104
105
106
107
108
109
110
111
/****************************************************************************
 *
 *   Copyright (C) 2013 PX4 Development Team. All rights reserved.
 *
 * Redistribution and use in source and binary forms, with or without
 * modification, are permitted provided that the following conditions
 * are met:
 *
 * 1. Redistributions of source code must retain the above copyright
 *    notice, this list of conditions and the following disclaimer.
 * 2. Redistributions in binary form must reproduce the above copyright
 *    notice, this list of conditions and the following disclaimer in
 *    the documentation and/or other materials provided with the
 *    distribution.
 * 3. Neither the name PX4 nor the names of its contributors may be
 *    used to endorse or promote products derived from this software
 *    without specific prior written permission.
 *
 * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
 * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
 * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
 * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
 * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
 * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
 * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
 * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
 * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
 * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
 * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
 * POSSIBILITY OF SUCH DAMAGE.
 *
 ****************************************************************************/

/**
 * @file airspeed_calibration.c
 * Airspeed sensor calibration routine
 */

#include "airspeed_calibration.h"
#include "commander_helper.h"

#include <stdio.h>
#include <poll.h>
#include <math.h>
#include <drivers/drv_hrt.h>
#include <uORB/topics/sensor_combined.h>
#include <uORB/topics/differential_pressure.h>
#include <mavlink/mavlink_log.h>
#include <systemlib/param/param.h>
#include <systemlib/err.h>

void do_airspeed_calibration(int mavlink_fd)
{
	/* give directions */
	mavlink_log_info(mavlink_fd, "airspeed calibration starting, keep it still");

	const int calibration_count = 2500;

	int diff_pres_sub = orb_subscribe(ORB_ID(differential_pressure));
	struct differential_pressure_s diff_pres;

	int calibration_counter = 0;
	float diff_pres_offset = 0.0f;

	while (calibration_counter < calibration_count) {

		/* wait blocking for new data */
		struct pollfd fds[1] = { { .fd = diff_pres_sub, .events = POLLIN } };

		int poll_ret = poll(fds, 1, 1000);

		if (poll_ret) {
			orb_copy(ORB_ID(differential_pressure), diff_pres_sub, &diff_pres);
			diff_pres_offset += diff_pres.differential_pressure_pa;
			calibration_counter++;

		} else if (poll_ret == 0) {
			/* any poll failure for 1s is a reason to abort */
			mavlink_log_info(mavlink_fd, "airspeed calibration aborted");
			return;
		}
	}

	diff_pres_offset = diff_pres_offset / calibration_count;

	if (isfinite(diff_pres_offset)) {

		if (param_set(param_find("SENS_DPRES_OFF"), &(diff_pres_offset))) {
			mavlink_log_critical(mavlink_fd, "Setting offs failed!");
		}

		/* auto-save to EEPROM */
		int save_ret = param_save_default();

		if (save_ret != 0) {
			warn("WARNING: auto-save of params to storage failed");
		}

		//char buf[50];
		//sprintf(buf, "[cmd] accel cal: x:%8.4f y:%8.4f z:%8.4f\n", (double)accel_offset[0], (double)accel_offset[1], (double)accel_offset[2]);
		//mavlink_log_info(mavlink_fd, buf);
		mavlink_log_info(mavlink_fd, "airspeed calibration done");

		tune_positive();

	} else {
		mavlink_log_info(mavlink_fd, "airspeed calibration FAILED (NaN)");
	}

	close(diff_pres_sub);
}