Initial BeeBrain Support

This commit is contained in:
borisbstyle 2016-10-12 12:29:59 +02:00
parent c0e34c11e2
commit b08a9ac89c
9 changed files with 133 additions and 8 deletions

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@ -3,6 +3,7 @@ env:
# - PUBLISHMETA=True
# - PUBLISHDOCS=True
# - TARGET=AFROMINI
# - TARGET=BEEBRAIN
# - TARGET=AIORACERF3
# - TARGET=AIR32
# - TARGET=ALIENFLIGHTF1

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@ -11,6 +11,7 @@ targets=("PUBLISHMETA=True" \
"TARGET=OMNIBUS" \
"TARGET=NAZE" \
"TARGET=AFROMINI" \
"TARGET=BEEBRAIN" \
"TARGET=RMDO" \
"TARGET=SPARKY" \
"TARGET=MOTOLAB" \

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@ -1,3 +0,0 @@
obj/main/betaflight_NAZE.elf: file format elf32-little

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@ -253,6 +253,7 @@ static void resetPidProfile(pidProfile_t *pidProfile)
pidProfile->yawRateAccelLimit = 220;
pidProfile->rateAccelLimit = 0;
pidProfile->itermThrottleGain = 0;
pidProfile->levelSensitivity = 2.0f;
#ifdef GTUNE
pidProfile->gtune_lolimP[ROLL] = 10; // [0..200] Lower limit of ROLL P during G tune.

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@ -217,10 +217,10 @@ static void pidBetaflight(const pidProfile_t *pidProfile, uint16_t max_angle_inc
if ((FLIGHT_MODE(ANGLE_MODE) || FLIGHT_MODE(HORIZON_MODE)) && axis != YAW) {
// calculate error angle and limit the angle to the max inclination
#ifdef GPS
const float errorAngle = (constrain(2 * rcCommand[axis] + GPS_angle[axis], -((int) max_angle_inclination),
const float errorAngle = (constrainf(pidProfile->levelSensitivity * rcCommand[axis] + GPS_angle[axis], -((int) max_angle_inclination),
+max_angle_inclination) - attitude.raw[axis] + angleTrim->raw[axis]) / 10.0f; // 16 bits is ok here
#else
const float errorAngle = (constrain(2 * rcCommand[axis], -((int) max_angle_inclination),
const float errorAngle = (constrainf(pidProfile->levelSensitivity * rcCommand[axis], -((int) max_angle_inclination),
+max_angle_inclination) - attitude.raw[axis] + angleTrim->raw[axis]) / 10.0f; // 16 bits is ok here
#endif
if (FLIGHT_MODE(ANGLE_MODE)) {

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@ -96,6 +96,7 @@ typedef struct pidProfile_s {
uint8_t dtermSetpointWeight; // Setpoint weight for Dterm (0= measurement, 1= full error, 1 > agressive derivative)
uint16_t yawRateAccelLimit; // yaw accel limiter for deg/sec/ms
uint16_t rateAccelLimit; // accel limiter roll/pitch deg/sec/ms
float levelSensitivity;
#ifdef GTUNE
uint8_t gtune_lolimP[3]; // [0..200] Lower limit of P during G tune

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@ -890,6 +890,8 @@ const clivalue_t valueTable[] = {
{ "i_vel", VAR_UINT8 | PROFILE_VALUE, &masterConfig.profile[0].pidProfile.I8[PIDVEL], .config.minmax = { 0, 200 } },
{ "d_vel", VAR_UINT8 | PROFILE_VALUE, &masterConfig.profile[0].pidProfile.D8[PIDVEL], .config.minmax = { 0, 200 } },
{ "level_sensitivity", VAR_FLOAT | PROFILE_VALUE, &masterConfig.profile[0].pidProfile.levelSensitivity, .config.minmax = { 0.1, 3.0 } },
#ifdef BLACKBOX
{ "blackbox_rate_num", VAR_UINT8 | MASTER_VALUE, &masterConfig.blackbox_rate_num, .config.minmax = { 1, 32 } },
{ "blackbox_rate_denom", VAR_UINT8 | MASTER_VALUE, &masterConfig.blackbox_rate_denom, .config.minmax = { 1, 32 } },

115
src/main/target/NAZE/config.c Executable file
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@ -0,0 +1,115 @@
/*
* This file is part of Cleanflight.
*
* Cleanflight is free software: you can redistribute it and/or modify
* it under the terms of the GNU General Public License as published by
* the Free Software Foundation, either version 3 of the License, or
* (at your option) any later version.
*
* Cleanflight is distributed in the hope that it will be useful,
* but WITHOUT ANY WARRANTY; without even the implied warranty of
* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
* GNU General Public License for more details.
*
* You should have received a copy of the GNU General Public License
* along with Cleanflight. If not, see <http://www.gnu.org/licenses/>.
*/
#include <stdint.h>
#include <platform.h>
#include "build_config.h"
#include "blackbox/blackbox_io.h"
#include "common/color.h"
#include "common/axis.h"
#include "common/filter.h"
#include "drivers/sensor.h"
#include "drivers/accgyro.h"
#include "drivers/system.h"
#include "drivers/timer.h"
#include "drivers/pwm_rx.h"
#include "drivers/serial.h"
#include "drivers/pwm_output.h"
#include "drivers/io.h"
#include "drivers/pwm_mapping.h"
#include "sensors/sensors.h"
#include "sensors/gyro.h"
#include "sensors/acceleration.h"
#include "sensors/barometer.h"
#include "sensors/boardalignment.h"
#include "sensors/battery.h"
#include "io/beeper.h"
#include "io/serial.h"
#include "io/gimbal.h"
#include "io/escservo.h"
#include "io/rc_controls.h"
#include "io/rc_curves.h"
#include "io/ledstrip.h"
#include "rx/rx.h"
#include "telemetry/telemetry.h"
#include "flight/mixer.h"
#include "flight/pid.h"
#include "flight/imu.h"
#include "flight/failsafe.h"
#include "flight/altitudehold.h"
#include "flight/navigation.h"
#include "config/runtime_config.h"
#include "config/config.h"
#include "config/config_profile.h"
#include "config/config_master.h"
#ifdef BEEBRAIN
// alternative defaults settings for Beebrain target
void targetConfiguration(master_t *config)
{
config->motor_pwm_rate = 4000;
config->failsafeConfig.failsafe_delay = 2;
config->failsafeConfig.failsafe_off_delay = 0;
config->escAndServoConfig.minthrottle = 1049;
config->gyro_lpf = 1;
config->gyro_soft_lpf_hz = 100;
config->gyro_soft_notch_hz_1 = 0;
for (int channel = 0; channel < NON_AUX_CHANNEL_COUNT; channel++) {
config->rxConfig.channelRanges[channel].min = 1180;
config->rxConfig.channelRanges[channel].max = 1860;
}
for (int profileId = 0; profileId < 2; profileId++) {
config->profile[profileId].pidProfile.P8[ROLL] = 55;
config->profile[profileId].pidProfile.I8[ROLL] = 40;
config->profile[profileId].pidProfile.D8[ROLL] = 20;
config->profile[profileId].pidProfile.P8[PITCH] = 55;
config->profile[profileId].pidProfile.I8[PITCH] = 40;
config->profile[profileId].pidProfile.D8[PITCH] = 20;
config->profile[profileId].pidProfile.P8[YAW] = 180;
config->profile[profileId].pidProfile.I8[YAW] = 45;
config->profile[profileId].pidProfile.P8[PIDLEVEL] = 50;
config->profile[profileId].pidProfile.D8[PIDLEVEL] = 50;
config->profile[profileId].pidProfile.levelSensitivity = 1.0f;
for (int rateProfileId = 0; rateProfileId < MAX_RATEPROFILES; rateProfileId++) {
config->profile[profileId].controlRateProfile[rateProfileId].rcRate8 = 120;
config->profile[profileId].controlRateProfile[rateProfileId].rcYawRate8 = 120;
config->profile[profileId].controlRateProfile[rateProfileId].rates[ROLL] = 99;
config->profile[profileId].controlRateProfile[rateProfileId].rates[PITCH] = 99;
config->profile[profileId].controlRateProfile[rateProfileId].rates[YAW] = 99;
config->profile[profileId].pidProfile.setpointRelaxRatio = 100;
}
}
}
#endif

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@ -17,7 +17,6 @@
#pragma once
#define TARGET_BOARD_IDENTIFIER "AFNA" // AFroNAze - NAZE might be considered misleading on Naze clones like the flip32.
#define USE_HARDWARE_REVISION_DETECTION
#define BOARD_HAS_VOLTAGE_DIVIDER
@ -25,9 +24,17 @@
#define LED0 PB3
#define LED1 PB4
#define BEEPER PA12
#ifdef AFROMINI
#define BEEPER PA1
#if defined(AFROMINI)
#define BEEPER_INVERTED
#define TARGET_BOARD_IDENTIFIER "AFMN"
#elif defined(BEEBRAIN)
#define BRUSHED_MOTORS
#define TARGET_BOARD_IDENTIFIER "BEBR"
#define TARGET_CONFIG
#else
#define TARGET_BOARD_IDENTIFIER "AFNA"
#endif
#define BARO_XCLR_PIN PC13