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Normalize all the line endings
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396 changed files with 158300 additions and 158300 deletions
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@ -1,265 +1,265 @@
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/*
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* This file is part of Cleanflight.
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*
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* Cleanflight is free software: you can redistribute it and/or modify
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* it under the terms of the GNU General Public License as published by
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* the Free Software Foundation, either version 3 of the License, or
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* (at your option) any later version.
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*
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* Cleanflight is distributed in the hope that it will be useful,
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* but WITHOUT ANY WARRANTY; without even the implied warranty of
|
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* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
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* GNU General Public License for more details.
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*
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* You should have received a copy of the GNU General Public License
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* along with Cleanflight. If not, see <http://www.gnu.org/licenses/>.
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*/
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#include <stdbool.h>
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#include <stdint.h>
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#include <string.h>
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#include <math.h>
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#include "common/axis.h"
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#include "common/maths.h"
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#include "config/config.h"
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#include "config/runtime_config.h"
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#include "flight/flight.h"
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#include "drivers/accgyro.h"
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#include "sensors/sensors.h"
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#include "sensors/gyro.h"
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#include "sensors/acceleration.h"
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#include "io/gps.h"
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#include "mw.h"
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#include "rx/rx.h"
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#include "io/rc_controls.h"
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int16_t rcCommand[4]; // interval [1000;2000] for THROTTLE and [-500;+500] for ROLL/PITCH/YAW
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// each entry in the array is a bitmask, 3 bits per aux channel (only aux 1 to 4), aux1 is first, each bit corresponds to an rc channel reading
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// bit 1 - stick LOW
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// bit 2 - stick MIDDLE
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// bit 3 - stick HIGH
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// an option is enabled when ANY channel has an appropriate reading corresponding to the bit.
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// an option is disabled when NO channel has an appropriate reading corresponding to the bit.
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// example: 110000000001 - option is only enabled when AUX1 is LOW or AUX4 is MEDIUM or HIGH.
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uint8_t rcOptions[CHECKBOX_ITEM_COUNT];
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bool areSticksInApModePosition(uint16_t ap_mode)
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{
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return abs(rcCommand[ROLL]) < ap_mode && abs(rcCommand[PITCH]) < ap_mode;
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}
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throttleStatus_e calculateThrottleStatus(rxConfig_t *rxConfig, uint16_t deadband3d_throttle)
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{
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if (feature(FEATURE_3D) && (rcData[THROTTLE] > (rxConfig->midrc - deadband3d_throttle) && rcData[THROTTLE] < (rxConfig->midrc + deadband3d_throttle)))
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return THROTTLE_LOW;
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else if (!feature(FEATURE_3D) && (rcData[THROTTLE] < rxConfig->mincheck))
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return THROTTLE_LOW;
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return THROTTLE_HIGH;
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}
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void processRcStickPositions(rxConfig_t *rxConfig, throttleStatus_e throttleStatus, uint32_t *activate, bool retarded_arm, bool disarm_kill_switch)
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{
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static uint8_t rcDelayCommand; // this indicates the number of time (multiple of RC measurement at 50Hz) the sticks must be maintained to run or switch off motors
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static uint8_t rcSticks; // this hold sticks position for command combos
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uint8_t stTmp = 0;
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int i;
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// ------------------ STICKS COMMAND HANDLER --------------------
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// checking sticks positions
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for (i = 0; i < 4; i++) {
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stTmp >>= 2;
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if (rcData[i] > rxConfig->mincheck)
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stTmp |= 0x80; // check for MIN
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if (rcData[i] < rxConfig->maxcheck)
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stTmp |= 0x40; // check for MAX
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}
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if (stTmp == rcSticks) {
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if (rcDelayCommand < 250)
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rcDelayCommand++;
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} else
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rcDelayCommand = 0;
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rcSticks = stTmp;
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// perform actions
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if (activate[BOXARM] > 0) {
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if (rcOptions[BOXARM]) {
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// Arming via ARM BOX
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if (throttleStatus == THROTTLE_LOW) {
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if (ARMING_FLAG(OK_TO_ARM)) {
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mwArm();
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}
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}
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} else {
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// Disarming via ARM BOX
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if (ARMING_FLAG(ARMED)) {
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if (disarm_kill_switch) {
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mwDisarm();
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} else if (throttleStatus == THROTTLE_LOW) {
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mwDisarm();
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}
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}
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}
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}
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if (rcDelayCommand != 20) {
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return;
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}
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if (ARMING_FLAG(ARMED)) {
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// actions during armed
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// Disarm on throttle down + yaw
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if (activate[BOXARM] == 0 && (rcSticks == THR_LO + YAW_LO + PIT_CE + ROL_CE))
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mwDisarm();
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// Disarm on roll (only when retarded_arm is enabled)
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if (retarded_arm && activate[BOXARM] == 0 && (rcSticks == THR_LO + YAW_CE + PIT_CE + ROL_LO))
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mwDisarm();
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return;
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}
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// actions during not armed
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i = 0;
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if (rcSticks == THR_LO + YAW_LO + PIT_LO + ROL_CE) {
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// GYRO calibration
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gyroSetCalibrationCycles(CALIBRATING_GYRO_CYCLES);
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#ifdef GPS
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if (feature(FEATURE_GPS)) {
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GPS_reset_home_position();
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}
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#endif
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#ifdef BARO
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if (sensors(SENSOR_BARO))
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baroSetCalibrationCycles(10); // calibrate baro to new ground level (10 * 25 ms = ~250 ms non blocking)
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#endif
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if (!sensors(SENSOR_MAG))
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heading = 0; // reset heading to zero after gyro calibration
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return;
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}
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if (feature(FEATURE_INFLIGHT_ACC_CAL) && (rcSticks == THR_LO + YAW_LO + PIT_HI + ROL_HI)) {
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// Inflight ACC Calibration
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handleInflightCalibrationStickPosition();
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return;
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}
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// Multiple configuration profiles
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if (rcSticks == THR_LO + YAW_LO + PIT_CE + ROL_LO) // ROLL left -> Profile 1
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i = 1;
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else if (rcSticks == THR_LO + YAW_LO + PIT_HI + ROL_CE) // PITCH up -> Profile 2
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i = 2;
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else if (rcSticks == THR_LO + YAW_LO + PIT_CE + ROL_HI) // ROLL right -> Profile 3
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i = 3;
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if (i) {
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changeProfile(i - 1);
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return;
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}
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if (activate[BOXARM] == 0 && (rcSticks == THR_LO + YAW_HI + PIT_CE + ROL_CE)) {
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// Arm via YAW
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mwArm();
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return;
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}
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if (retarded_arm && activate[BOXARM] == 0 && (rcSticks == THR_LO + YAW_CE + PIT_CE + ROL_HI)) {
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// Arm via ROLL
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mwArm();
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return;
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}
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if (rcSticks == THR_HI + YAW_LO + PIT_LO + ROL_CE) {
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// Calibrating Acc
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accSetCalibrationCycles(CALIBRATING_ACC_CYCLES);
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return;
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}
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if (rcSticks == THR_HI + YAW_HI + PIT_LO + ROL_CE) {
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// Calibrating Mag
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ENABLE_STATE(CALIBRATE_MAG);
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return;
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}
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// Accelerometer Trim
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rollAndPitchTrims_t accelerometerTrimsDelta;
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memset(&accelerometerTrimsDelta, 0, sizeof(accelerometerTrimsDelta));
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bool shouldApplyRollAndPitchTrimDelta = false;
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if (rcSticks == THR_HI + YAW_CE + PIT_HI + ROL_CE) {
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accelerometerTrimsDelta.values.pitch = 2;
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shouldApplyRollAndPitchTrimDelta = true;
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} else if (rcSticks == THR_HI + YAW_CE + PIT_LO + ROL_CE) {
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accelerometerTrimsDelta.values.pitch = -2;
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shouldApplyRollAndPitchTrimDelta = true;
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} else if (rcSticks == THR_HI + YAW_CE + PIT_CE + ROL_HI) {
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accelerometerTrimsDelta.values.roll = 2;
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shouldApplyRollAndPitchTrimDelta = true;
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} else if (rcSticks == THR_HI + YAW_CE + PIT_CE + ROL_LO) {
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accelerometerTrimsDelta.values.roll = -2;
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shouldApplyRollAndPitchTrimDelta = true;
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}
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if (shouldApplyRollAndPitchTrimDelta) {
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applyAndSaveAccelerometerTrimsDelta(&accelerometerTrimsDelta);
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rcDelayCommand = 0; // allow autorepetition
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return;
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}
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}
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#define MAX_AUX_STATE_CHANNELS 8
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void updateRcOptions(uint32_t *activate)
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{
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// auxState is a bitmask, 3 bits per channel.
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// lower 16 bits contain aux 4 to 1 (msb to lsb)
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// upper 16 bits contain aux 8 to 5 (msb to lsb)
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//
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// the three bits are as follows:
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// bit 1 is SET when the stick is less than 1300
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// bit 2 is SET when the stick is between 1300 and 1700
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// bit 3 is SET when the stick is above 1700
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// if the value is 1300 or 1700 NONE of the three bits are set.
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int i;
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uint32_t auxState = 0;
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uint8_t shift = 0;
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int8_t chunkOffset = 0;
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for (i = 0; i < rxRuntimeConfig.auxChannelCount && i < MAX_AUX_STATE_CHANNELS; i++) {
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if (i > 0 && i % 4 == 0) {
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chunkOffset -= 4;
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shift += 16;
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}
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uint8_t bitIndex = 3 * (i + chunkOffset);
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uint32_t temp =
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(rcData[AUX1 + i] < 1300) << bitIndex |
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(1300 < rcData[AUX1 + i] && rcData[AUX1 + i] < 1700) << (bitIndex + 1) |
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(rcData[AUX1 + i] > 1700) << (bitIndex + 2);
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auxState |= temp << shift;
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}
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for (i = 0; i < CHECKBOX_ITEM_COUNT; i++)
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rcOptions[i] = (auxState & activate[i]) > 0;
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}
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/*
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* This file is part of Cleanflight.
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*
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* Cleanflight is free software: you can redistribute it and/or modify
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* it under the terms of the GNU General Public License as published by
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* the Free Software Foundation, either version 3 of the License, or
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* (at your option) any later version.
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*
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* Cleanflight is distributed in the hope that it will be useful,
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* but WITHOUT ANY WARRANTY; without even the implied warranty of
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* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
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* GNU General Public License for more details.
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*
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* You should have received a copy of the GNU General Public License
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* along with Cleanflight. If not, see <http://www.gnu.org/licenses/>.
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*/
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#include <stdbool.h>
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#include <stdint.h>
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#include <string.h>
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#include <math.h>
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#include "common/axis.h"
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#include "common/maths.h"
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#include "config/config.h"
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#include "config/runtime_config.h"
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#include "flight/flight.h"
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#include "drivers/accgyro.h"
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#include "sensors/sensors.h"
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#include "sensors/gyro.h"
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#include "sensors/acceleration.h"
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#include "io/gps.h"
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#include "mw.h"
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#include "rx/rx.h"
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#include "io/rc_controls.h"
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int16_t rcCommand[4]; // interval [1000;2000] for THROTTLE and [-500;+500] for ROLL/PITCH/YAW
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// each entry in the array is a bitmask, 3 bits per aux channel (only aux 1 to 4), aux1 is first, each bit corresponds to an rc channel reading
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// bit 1 - stick LOW
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// bit 2 - stick MIDDLE
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// bit 3 - stick HIGH
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// an option is enabled when ANY channel has an appropriate reading corresponding to the bit.
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// an option is disabled when NO channel has an appropriate reading corresponding to the bit.
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// example: 110000000001 - option is only enabled when AUX1 is LOW or AUX4 is MEDIUM or HIGH.
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uint8_t rcOptions[CHECKBOX_ITEM_COUNT];
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bool areSticksInApModePosition(uint16_t ap_mode)
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{
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return abs(rcCommand[ROLL]) < ap_mode && abs(rcCommand[PITCH]) < ap_mode;
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}
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throttleStatus_e calculateThrottleStatus(rxConfig_t *rxConfig, uint16_t deadband3d_throttle)
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{
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if (feature(FEATURE_3D) && (rcData[THROTTLE] > (rxConfig->midrc - deadband3d_throttle) && rcData[THROTTLE] < (rxConfig->midrc + deadband3d_throttle)))
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return THROTTLE_LOW;
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else if (!feature(FEATURE_3D) && (rcData[THROTTLE] < rxConfig->mincheck))
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return THROTTLE_LOW;
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return THROTTLE_HIGH;
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}
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void processRcStickPositions(rxConfig_t *rxConfig, throttleStatus_e throttleStatus, uint32_t *activate, bool retarded_arm, bool disarm_kill_switch)
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{
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static uint8_t rcDelayCommand; // this indicates the number of time (multiple of RC measurement at 50Hz) the sticks must be maintained to run or switch off motors
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static uint8_t rcSticks; // this hold sticks position for command combos
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uint8_t stTmp = 0;
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int i;
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// ------------------ STICKS COMMAND HANDLER --------------------
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// checking sticks positions
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for (i = 0; i < 4; i++) {
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stTmp >>= 2;
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if (rcData[i] > rxConfig->mincheck)
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stTmp |= 0x80; // check for MIN
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if (rcData[i] < rxConfig->maxcheck)
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stTmp |= 0x40; // check for MAX
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}
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if (stTmp == rcSticks) {
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if (rcDelayCommand < 250)
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rcDelayCommand++;
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} else
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rcDelayCommand = 0;
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rcSticks = stTmp;
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// perform actions
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if (activate[BOXARM] > 0) {
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if (rcOptions[BOXARM]) {
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// Arming via ARM BOX
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if (throttleStatus == THROTTLE_LOW) {
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if (ARMING_FLAG(OK_TO_ARM)) {
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mwArm();
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}
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}
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} else {
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// Disarming via ARM BOX
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if (ARMING_FLAG(ARMED)) {
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if (disarm_kill_switch) {
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mwDisarm();
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} else if (throttleStatus == THROTTLE_LOW) {
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mwDisarm();
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}
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}
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}
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}
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if (rcDelayCommand != 20) {
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return;
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}
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if (ARMING_FLAG(ARMED)) {
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// actions during armed
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// Disarm on throttle down + yaw
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if (activate[BOXARM] == 0 && (rcSticks == THR_LO + YAW_LO + PIT_CE + ROL_CE))
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mwDisarm();
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// Disarm on roll (only when retarded_arm is enabled)
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if (retarded_arm && activate[BOXARM] == 0 && (rcSticks == THR_LO + YAW_CE + PIT_CE + ROL_LO))
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mwDisarm();
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return;
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}
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// actions during not armed
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i = 0;
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if (rcSticks == THR_LO + YAW_LO + PIT_LO + ROL_CE) {
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// GYRO calibration
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gyroSetCalibrationCycles(CALIBRATING_GYRO_CYCLES);
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#ifdef GPS
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if (feature(FEATURE_GPS)) {
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GPS_reset_home_position();
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}
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||||
#endif
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#ifdef BARO
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if (sensors(SENSOR_BARO))
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baroSetCalibrationCycles(10); // calibrate baro to new ground level (10 * 25 ms = ~250 ms non blocking)
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||||
#endif
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||||
if (!sensors(SENSOR_MAG))
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heading = 0; // reset heading to zero after gyro calibration
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||||
return;
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}
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if (feature(FEATURE_INFLIGHT_ACC_CAL) && (rcSticks == THR_LO + YAW_LO + PIT_HI + ROL_HI)) {
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// Inflight ACC Calibration
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handleInflightCalibrationStickPosition();
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return;
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}
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// Multiple configuration profiles
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if (rcSticks == THR_LO + YAW_LO + PIT_CE + ROL_LO) // ROLL left -> Profile 1
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i = 1;
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else if (rcSticks == THR_LO + YAW_LO + PIT_HI + ROL_CE) // PITCH up -> Profile 2
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i = 2;
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else if (rcSticks == THR_LO + YAW_LO + PIT_CE + ROL_HI) // ROLL right -> Profile 3
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i = 3;
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if (i) {
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changeProfile(i - 1);
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||||
return;
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||||
}
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||||
|
||||
if (activate[BOXARM] == 0 && (rcSticks == THR_LO + YAW_HI + PIT_CE + ROL_CE)) {
|
||||
// Arm via YAW
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mwArm();
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||||
return;
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||||
}
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||||
|
||||
if (retarded_arm && activate[BOXARM] == 0 && (rcSticks == THR_LO + YAW_CE + PIT_CE + ROL_HI)) {
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// Arm via ROLL
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mwArm();
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return;
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}
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||||
|
||||
if (rcSticks == THR_HI + YAW_LO + PIT_LO + ROL_CE) {
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||||
// Calibrating Acc
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||||
accSetCalibrationCycles(CALIBRATING_ACC_CYCLES);
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||||
return;
|
||||
}
|
||||
|
||||
|
||||
if (rcSticks == THR_HI + YAW_HI + PIT_LO + ROL_CE) {
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||||
// Calibrating Mag
|
||||
ENABLE_STATE(CALIBRATE_MAG);
|
||||
return;
|
||||
}
|
||||
|
||||
|
||||
// Accelerometer Trim
|
||||
|
||||
rollAndPitchTrims_t accelerometerTrimsDelta;
|
||||
memset(&accelerometerTrimsDelta, 0, sizeof(accelerometerTrimsDelta));
|
||||
|
||||
bool shouldApplyRollAndPitchTrimDelta = false;
|
||||
if (rcSticks == THR_HI + YAW_CE + PIT_HI + ROL_CE) {
|
||||
accelerometerTrimsDelta.values.pitch = 2;
|
||||
shouldApplyRollAndPitchTrimDelta = true;
|
||||
} else if (rcSticks == THR_HI + YAW_CE + PIT_LO + ROL_CE) {
|
||||
accelerometerTrimsDelta.values.pitch = -2;
|
||||
shouldApplyRollAndPitchTrimDelta = true;
|
||||
} else if (rcSticks == THR_HI + YAW_CE + PIT_CE + ROL_HI) {
|
||||
accelerometerTrimsDelta.values.roll = 2;
|
||||
shouldApplyRollAndPitchTrimDelta = true;
|
||||
} else if (rcSticks == THR_HI + YAW_CE + PIT_CE + ROL_LO) {
|
||||
accelerometerTrimsDelta.values.roll = -2;
|
||||
shouldApplyRollAndPitchTrimDelta = true;
|
||||
}
|
||||
if (shouldApplyRollAndPitchTrimDelta) {
|
||||
applyAndSaveAccelerometerTrimsDelta(&accelerometerTrimsDelta);
|
||||
rcDelayCommand = 0; // allow autorepetition
|
||||
return;
|
||||
}
|
||||
}
|
||||
|
||||
#define MAX_AUX_STATE_CHANNELS 8
|
||||
|
||||
void updateRcOptions(uint32_t *activate)
|
||||
{
|
||||
// auxState is a bitmask, 3 bits per channel.
|
||||
// lower 16 bits contain aux 4 to 1 (msb to lsb)
|
||||
// upper 16 bits contain aux 8 to 5 (msb to lsb)
|
||||
//
|
||||
// the three bits are as follows:
|
||||
// bit 1 is SET when the stick is less than 1300
|
||||
// bit 2 is SET when the stick is between 1300 and 1700
|
||||
// bit 3 is SET when the stick is above 1700
|
||||
|
||||
// if the value is 1300 or 1700 NONE of the three bits are set.
|
||||
|
||||
int i;
|
||||
uint32_t auxState = 0;
|
||||
uint8_t shift = 0;
|
||||
int8_t chunkOffset = 0;
|
||||
|
||||
for (i = 0; i < rxRuntimeConfig.auxChannelCount && i < MAX_AUX_STATE_CHANNELS; i++) {
|
||||
if (i > 0 && i % 4 == 0) {
|
||||
chunkOffset -= 4;
|
||||
shift += 16;
|
||||
}
|
||||
|
||||
uint8_t bitIndex = 3 * (i + chunkOffset);
|
||||
|
||||
uint32_t temp =
|
||||
(rcData[AUX1 + i] < 1300) << bitIndex |
|
||||
(1300 < rcData[AUX1 + i] && rcData[AUX1 + i] < 1700) << (bitIndex + 1) |
|
||||
(rcData[AUX1 + i] > 1700) << (bitIndex + 2);
|
||||
|
||||
auxState |= temp << shift;
|
||||
}
|
||||
|
||||
for (i = 0; i < CHECKBOX_ITEM_COUNT; i++)
|
||||
rcOptions[i] = (auxState & activate[i]) > 0;
|
||||
}
|
||||
|
|
Loading…
Add table
Add a link
Reference in a new issue