確認用

Dependencies:   HCSR04_2 MPU6050_2 mbed SDFileSystem3

Fork of Autoflight2018_29 by 航空研究会

Revision:
0:17f575135219
Child:
1:f383708a5a52
--- /dev/null	Thu Jan 01 00:00:00 1970 +0000
+++ b/main.cpp	Fri Sep 07 04:11:48 2018 +0000
@@ -0,0 +1,1216 @@
+//mbed
+#include "mbed.h"
+#include "FATFileSystem.h"
+#include "SDFileSystem.h"
+//C
+#include "math.h"
+//sensor
+#include "MPU6050_DMP6.h"
+//#include "MPU9250.h"
+//#include "BMP280.h"
+#include "hcsr04.h"
+//device
+#include "sbus.h"
+//config
+#include "SkipperSv2.h"
+#include "falfalla.h"
+//other
+#include "pid.h"
+
+#define DEBUG_SEMIAUTO 0
+#define DEBUG_PRINT_INLOOP 1
+
+#define KP_ELE 2.0
+#define KI_ELE 0.0
+#define KD_ELE 0.0
+#define KP_RUD 3.0
+#define KI_RUD 0.0
+#define KD_RUD 0.0
+
+#define GAIN_CONTROLVALUE_TO_PWM 3.0
+
+#define RIGHT_ROLL -12.0
+#define RIGHT_PITCH -5.0
+#define LEFT_ROLL 12.0
+#define LEFT_PITCH -5.0
+#define STRAIGHT_ROLL 4.0
+#define STRAIGHT_PITCH 3.0
+#define TAKEOFF_THR 0.8
+#define LOOP_THR 0.6
+
+#define RIGHT_ROLL_SHORT -12.0
+#define RIGHT_PITCH_SHORT -5.0
+#define LEFT_ROLL_SHORT 12.0
+#define LEFT_PITCH_SHORT -5.0
+
+#define GLIDE_ROLL -12.0
+#define GLIDE_PITCH -3.0
+
+//コンパスキャリブレーション
+//SkipperS2基板
+/*
+#define MAGBIAS_X -35.0
+#define MAGBIAS_Y 535.0
+#define MAGBIAS_Z -50.0
+*/
+//S2v2 1番基板
+#define MAGBIAS_X 395.0
+#define MAGBIAS_Y 505.0
+#define MAGBIAS_Z -725.0
+//S2v2 2番基板
+/*
+#define MAGBIAS_X 185.0
+#define MAGBIAS_Y 220.0
+#define MAGBIAS_Z -350.0
+*/
+
+#define ELEMENT 1
+#define LIMIT_STRAIGHT_YAW 5.0 
+#define THRESHOLD_TURNINGRADIUS_YAW 60.0 
+#define ALLOWHEIGHT 15
+
+#ifndef PI
+#define PI 3.14159265358979
+#endif
+
+const int16_t lengthdivpwm = 320; 
+const int16_t changeModeCount = 6;
+
+const float trim[4] = {Trim_Falfalla[0],Trim_Falfalla[1],Trim_Falfalla[2],Trim_Falfalla[3]};
+const float expMax[4] = {ExpMax_Falfalla[0],ExpMax_Falfalla[1],ExpMax_Falfalla[2],ExpMax_Falfalla[3]};
+const float expMin[4] = {ExpMin_Falfalla[0],ExpMin_Falfalla[1],ExpMin_Falfalla[2],ExpMin_Falfalla[3]};
+const int16_t reverce[4] = {ExpMin_Falfalla[0],Reverce_falfalla[1],Reverce_falfalla[2],Reverce_falfalla[3]};
+
+SBUS sbus(PA_9, PA_10); //SBUS
+
+PwmOut servo1(PC_6); // TIM3_CH1  //old echo
+PwmOut servo2(PC_7); // TIM3_CH2    //PC_7
+PwmOut servo3(PB_0); // TIM3_CH3
+PwmOut servo4(PB_1); // TIM3_CH4
+PwmOut servo5(PB_6); // TIM4_CH1
+PwmOut servo6(PB_7); // TIM4_CH2  //old trigger
+//PwmOut servo7(PB_8); // TIM4_CH3    //PB_8 new echo
+//PwmOut servo8(PB_9); // TIM4_CH4   //new trigger
+
+RawSerial pc(PA_2,PA_3, 115200);    //tx,rx.baudrate pin;PA_2=UART2_TX, PA_3=UART2_RX
+SDFileSystem sd(PB_15, PB_14, PB_13, PB_12, "sd");
+
+DigitalOut led1(PA_0);  //黄色のコネクタ
+DigitalOut led2(PA_1);
+DigitalOut led3(PB_4); 
+DigitalOut led4(PB_5);
+
+//InterruptIn switch2(PC_14);
+MPU6050DMP6 mpu6050(PC_0,&pc); //割り込みピン,シリアルポインタ i2cのピン指定は MPU6050>>I2Cdev.h 内のdefine
+HCSR04 usensor(PB_9,PB_8); //trig,echo  9,8 
+
+PID pid_ELE(g_kpELE,g_kiELE,g_kdELE);
+PID pid_RUD(g_kpRUD,g_kiRUD,g_kdRUD);
+
+enum Channel{AIL_R, ELE, THR, RUD, DROP, AIL_L, Ch7, Ch8};
+enum Angle{ROLL, PITCH, YAW};   //yaw:北を0とした絶対角度
+enum OperationMode{StartUp, SemiAuto, RightLoop, LeftLoop, GoStraight, BombwithPC, ZERO, Moebius, Glide};
+enum BombingMode{Takeoff, Chicken, Transition, Approach};
+enum OutputStatus{Manual, Auto};
+
+static OutputStatus output_status = Manual;
+OperationMode operation_mode = StartUp;
+BombingMode bombing_mode = Takeoff;
+static int16_t autopwm[8] = {1500,1500,1180,1500,1392,1500};
+static int16_t trimpwm[6] = {1500,1500,1180,1500,1392,1500};
+int16_t maxpwm[6] = {1820,1820,1820,1820,1820,1820};
+int16_t minpwm[6] = {1180,1180,1180,1180,1180,1180};
+int16_t oldTHR = 1000;
+
+static float nowAngle[3] = {0,0,0};
+const float trimAngle[3] = {0.0, 0.0, 0.0};
+const float maxAngle[2] = {90, 90};
+const float minAngle[2] = {-90, -90};
+
+float FirstROLL = 0.0, FirstPITCH = 0.0 ,FirstYAW = 0.0;
+
+unsigned int g_distance;
+Ticker USsensor;
+static char g_buf[16];
+char g_landingcommand;
+float g_SerialTargetYAW;
+
+Timer t;
+Timeout RerurnChickenServo1;
+Timeout RerurnChickenServo2;
+
+/*-----関数のプロトタイプ宣言-----*/
+void setup();
+void loop();
+
+void Init_PWM();
+void Init_servo();              //サーボ初期化
+void Init_sbus();               //SBUS初期化
+void Init_sensors();
+void DisplayClock();            //クロック状態確認
+
+//センサの値取得
+void SensingMPU();
+void UpdateDist();
+
+//void offsetRollPitch(float FirstROLL, float FirstPITCH);
+//void TransYaw(float FirstYAW);
+float TranslateNewYaw(float beforeYaw,  float newzeroYaw);
+void UpdateTargetAngle(float targetAngle[3]);
+void CalculateControlValue(float targetAngle[3], float controlValue[3]);
+void UpdateAutoPWM(float controlValue[3]);
+void ConvertPWMintoRAD(float targetAngle[3]);
+inline float CalcRatio(float value, float trim, float limit);
+bool CheckSW_Up(Channel ch);
+int16_t ThresholdMaxMin(int16_t value, int16_t max, int16_t min);
+inline int16_t SetTHRinRatio(float ratio);
+
+//sbus割り込み
+void Update_PWM();              //マニュアル・自動モードのpwmデータを整形しpwm変数に入力
+void Output_PWM(int16_t pwm[6]);    //pwmをサーボへ出力
+
+//シリアル割り込み
+void SendSerial();   //1文字きたら送り返す
+void SendArray();
+void getSF_Serial();
+float ConvertByteintoFloat(char high, char low);
+
+//SD設定
+int GetParameter(FILE *fp, const char *paramName,char parameter[]);
+int SetOptions(float *g_kpELE, float *g_kiELE, float *g_kdELE,
+               float *g_kpRUD, float *g_kiRUD, float *g_kdRUD,
+               float *g_rightloopROLL, float *g_rightloopPITCH,
+               float *g_leftloopROLL, float *g_leftloopPITCH,
+               float *g_gostraightROLL, float *g_gostraightPITCH,
+               float *g_takeoffTHR, float *g_loopTHR,
+               float *g_rightloopROLLshort, float *g_rightloopPITCHshort,
+               float *g_leftloopROLLshort, float *g_leftloopPITCHshort,
+               float *g_glideloopROLL, float *g_glideloopPITCH);
+//switch2割り込み
+void ResetTrim();
+
+//自動操縦
+void UpdateTargetAngle_GoStraight(float targetAngle[3]);
+void UpdateTargetAngle_Rightloop(float targetAngle[3]);
+void UpdateTargetAngle_Rightloop_short(float targetAngle[3]);
+void UpdateTargetAngle_Leftloop(float targetAngle[3]);
+void UpdateTargetAngle_Leftloop_short(float targetAngle[3]);
+void UpdateTargetAngle_Moebius(float targetAngle[3]);
+void UpdateTargetAngle_Glide(float targetAngle[3]);
+void UpdateTargetAngle_Takeoff(float targetAngle[3]);
+void UpdateTargetAngle_Approach(float targetAngle[3]);
+void Take_off_and_landing(float targetAngle[3]);
+
+int Rotate(float targetAngle[3], float TargetYAW);
+
+//投下
+void Chicken_Drop();
+void ReturnChickenServo1();
+void ReturnChickenServo2();
+
+//超音波による高度補正
+void checkHeight(float targetAngle[3]);
+void UpdateTargetAngle_NoseUP(float targetAngle[3]);
+void UpdateTargetAngle_NoseDOWN(float targetAngle[3]);
+
+//デバッグ用
+void DebugPrint();
+
+/*---関数のプロトタイプ宣言終わり---*/
+
+int main()
+{   
+    setup();
+    
+    
+    while(1){
+        
+        loop();
+        
+        if(!CheckSW_Up(Ch7)){
+            led3=0;
+        }else{
+            led3=1;
+        }
+    }
+    
+}
+
+void setup(){
+    //buzzer = 0;
+    led1 = 1;
+    led2 = 1;
+    led3 = 1;
+    led4 = 1;
+    
+    SetOptions(&g_kpELE, &g_kiELE, &g_kdELE,
+               &g_kpRUD, &g_kiRUD, &g_kdRUD,
+               &g_rightloopROLL, &g_rightloopPITCH,
+               &g_leftloopROLL, &g_leftloopPITCH,
+               &g_gostraightROLL, &g_gostraightPITCH,
+               &g_takeoffTHR, &g_loopTHR,
+               &g_rightloopROLLshort, &g_rightloopPITCHshort,
+               &g_leftloopROLLshort, &g_leftloopPITCHshort,
+               &g_glideloopROLL, &g_glideloopPITCH);    
+    
+        
+    Init_PWM();
+    Init_servo();
+    Init_sbus();    
+    Init_sensors();
+    //switch2.rise(ResetTrim);
+    pc.attach(getSF_Serial, Serial::RxIrq);
+    USsensor.attach(&UpdateDist, 0.05);
+    
+    NVIC_SetPriority(USART1_IRQn,0);
+    NVIC_SetPriority(EXTI0_IRQn,1);
+    NVIC_SetPriority(TIM5_IRQn,2);
+    NVIC_SetPriority(EXTI9_5_IRQn,3);
+    NVIC_SetPriority(USART2_IRQn,4);
+    DisplayClock();
+    t.start();
+    
+    
+    pc.printf("MPU calibration start\r\n");
+    
+    float offsetstart = t.read();
+    while(t.read() - offsetstart < 26){
+        SensingMPU();
+        for(uint8_t i=0; i<3; i++) pc.printf("%3.2f\t",nowAngle[i]);
+        pc.printf("\r\n");
+        led1 = !led1;
+        led2 = !led2;
+        led3 = !led3;
+        led4 = !led4;
+    }
+    
+    FirstROLL = nowAngle[ROLL];
+    FirstPITCH = nowAngle[PITCH];
+    nowAngle[ROLL] -=FirstROLL;
+    nowAngle[PITCH] -=FirstPITCH;
+    
+    led1 = 0;
+    led2 = 0;
+    led3 = 0;
+    led4 = 0;
+    wait(0.2);
+    
+    
+    pc.printf("All initialized\r\n");
+}
+
+void loop(){
+    static float targetAngle[3] = {0.0, 0.0, 0.0}, controlValue[2] = {0.0, 0.0};
+
+    SensingMPU();
+    UpdateTargetAngle(targetAngle);
+    //Rotate(targetAngle, 30.0);
+    CalculateControlValue(targetAngle, controlValue);
+    UpdateAutoPWM(controlValue);
+    wait_ms(23);
+#if DEBUG_PRINT_INLOOP
+    DebugPrint();
+#endif
+}
+
+//サーボ初期化関数
+void Init_servo(){
+    
+    servo1.period_ms(14);
+    servo1.pulsewidth_us(trimpwm[AIL_R]);
+    
+    servo2.period_ms(14);
+    servo2.pulsewidth_us(trimpwm[ELE]);
+    
+    servo3.period_ms(14);
+    servo3.pulsewidth_us(trimpwm[THR]);
+    
+    servo4.period_ms(14);
+    servo4.pulsewidth_us(trimpwm[RUD]);
+    
+    servo5.period_ms(14);
+    servo5.pulsewidth_us(1392);
+
+    servo6.period_ms(14);
+    servo6.pulsewidth_us(trimpwm[AIL_L]);
+
+    pc.printf("servo initialized\r\n");
+}
+
+//Sbus初期化
+void Init_sbus(){
+    sbus.initialize();
+    sbus.setLastfuncPoint(Update_PWM);
+    sbus.startInterrupt();
+}
+
+void Init_sensors(){
+    if(mpu6050.setup() == -1){
+        pc.printf("failed initialize\r\n");
+        while(1){
+            led1 = 1; led2 = 0; led3 = 1; led4 = 0;
+            wait(1);
+            led1 = 0; led2 = 1; led3 = 0; led4 = 1;
+            wait(1);
+        }
+    }
+}
+
+void Init_PWM(){
+    for (uint8_t i = 0; i < 4; ++i){
+        trimpwm[i] = 1500 + (int16_t)(lengthdivpwm * (trim[i]/100));
+        maxpwm[i] = 1500 + (int16_t)(lengthdivpwm * (expMax[i]/100));
+        minpwm[i] = 1500 - (int16_t)(lengthdivpwm * (expMin[i]/100));
+    }
+    pc.printf("PWM initialized\r\n");
+}
+
+void DisplayClock(){
+    pc.printf("System Clock = %d[MHz]\r\n", HAL_RCC_GetSysClockFreq()/1000000);
+    pc.printf("HCLK Clock   = %d[MHz]\r\n", HAL_RCC_GetHCLKFreq()/1000000);
+    pc.printf("PCLK1 Clock  = %d[MHz]\r\n", HAL_RCC_GetPCLK1Freq()/1000000);
+    pc.printf("PCLK2 Clock  = %d[MHz]\r\n", HAL_RCC_GetPCLK2Freq()/1000000);
+    pc.printf("\r\n");
+}
+
+void UpdateTargetAngle(float targetAngle[3]){
+    static int16_t count_op = 0;
+#if DEBUG_SEMIAUTO    
+    switch(operation_mode){
+        case StartUp:
+            if(!CheckSW_Up(Ch7) && CheckSW_Up(Ch8)){
+                count_op++;
+                if(count_op > changeModeCount){
+                    operation_mode = SemiAuto;
+                    pc.printf("Goto SemiAuto mode\r\n");
+                    count_op = 0;
+                }
+            }else count_op = 0;
+            break;
+
+        case SemiAuto:
+        /*  大会用では以下のif文を入れてoperation_modeを変える
+            if(CheckSW_Up(Ch6)){
+                count_op++;
+                if(count_op>changeModeCount){
+                    output_status = XXX;
+                    led2 = 0;
+                    pc.printf("Goto XXX mode\r\n");
+                    count_op = 0;
+                }else count_op = 0;
+                ConvertPWMintoRAD(targetAngle);
+            }
+        */
+            ConvertPWMintoRAD(targetAngle);
+            break;
+
+        default:
+            operation_mode = SemiAuto;
+            break;
+    }
+
+#else
+
+    switch(operation_mode){
+        case StartUp:
+            if(!CheckSW_Up(Ch7) && !CheckSW_Up(Ch8)){        //ch7;自動・手動切り替え ch8;自動操縦モード切替
+                count_op++;
+                if(count_op > changeModeCount){
+                    operation_mode = RightLoop;
+                    pc.printf("Goto RightLoop mode\r\n");
+                    count_op = 0;
+                }
+            }else count_op = 0;
+            break;
+
+        case RightLoop:
+            if(!CheckSW_Up(Ch7) && CheckSW_Up(Ch8)){
+                count_op++;
+                if(count_op > changeModeCount){
+                    operation_mode = LeftLoop;
+                    pc.printf("Goto LeftLoop mode\r\n");
+                    count_op = 0;
+                }
+            }else count_op = 0;
+            UpdateTargetAngle_Rightloop(targetAngle);
+            
+            break;
+
+        case LeftLoop:
+            if(!CheckSW_Up(Ch7) && !CheckSW_Up(Ch8)){
+                count_op++;
+                if(count_op > changeModeCount){
+                    operation_mode = GoStraight;
+                    pc.printf("Goto GoStraight mode\r\n");
+                    count_op = 0;
+                }
+            }else count_op = 0;
+            UpdateTargetAngle_Leftloop(targetAngle);
+            break;
+        
+        case GoStraight:
+            if(!CheckSW_Up(Ch7) && CheckSW_Up(Ch8)){
+                count_op++;
+                if(count_op > changeModeCount){
+                    operation_mode = Moebius;
+                    pc.printf("Goto Moebius mode\r\n");
+                    count_op = 0;
+                }
+            }else count_op = 0;
+            UpdateTargetAngle_GoStraight(targetAngle);
+            break;
+
+        case Moebius:
+            if(!CheckSW_Up(Ch7) && !CheckSW_Up(Ch8)){
+                count_op++;
+                if(count_op > changeModeCount){
+                    operation_mode = Glide;
+                    pc.printf("Goto Glide mode\r\n");
+                    count_op = 0;
+                }
+            }else count_op = 0;
+            UpdateTargetAngle_Moebius(targetAngle);
+            break;
+
+        case Glide:
+            if(!CheckSW_Up(Ch7) && CheckSW_Up(Ch8)){
+                count_op++;
+                if(count_op > changeModeCount){
+                    operation_mode = BombwithPC;
+                    pc.printf("Goto Bombing mode\r\n");
+                    count_op = 0;
+                }
+            }else count_op = 0;
+            UpdateTargetAngle_Glide(targetAngle);
+            break;
+
+        case BombwithPC:
+            if(!CheckSW_Up(Ch7) && !CheckSW_Up(Ch8)){
+                count_op++;
+                if(count_op > changeModeCount){
+                    operation_mode = RightLoop;
+                    pc.printf("Goto RightLoop mode\r\n");
+                    count_op = 0;
+                }
+            }else count_op = 0;
+            Take_off_and_landing(targetAngle);
+            break;
+
+        default:
+            operation_mode = StartUp;
+            break;
+    }
+#endif
+
+    if(CheckSW_Up(Ch7)){
+        output_status = Auto;
+        led1 = 1;
+    }else{
+        output_status = Manual;
+        led1 = 0;
+    }
+}
+
+int GetParameter(FILE *fp, const char *paramName,char parameter[]){
+    int i=0, j=0;
+    int strmax = 200;
+    char str[strmax];
+
+    rewind(fp); //ファイル位置を先頭に
+    while(1){
+        if (fgets(str, strmax, fp) == NULL) {
+            return 0;
+        }
+        if (!strncmp(str, paramName, strlen(paramName))) {
+            while (str[i++] != '=') {}
+            while (str[i] != '\n') {
+                    parameter[j++] = str[i++];
+            }
+            parameter[j] = '\0';
+            return 1;
+        }
+    }
+    return 0;
+}
+
+
+//sdによる設定
+int SetOptions(float *g_kpELE, float *g_kiELE, float *g_kdELE,
+               float *g_kpRUD, float *g_kiRUD, float *g_kdRUD,
+               float *g_rightloopROLL, float *g_rightloopPITCH,
+               float *g_leftloopROLL, float *g_leftloopPITCH,
+               float *g_gostraightROLL, float *g_gostraightPITCH,
+               float *g_takeoffTHR, float *g_loopTHR,
+               float *g_rightloopROLLshort, float *g_rightloopPITCHshort,
+               float *g_leftloopROLLshort, float *g_leftloopPITCHshort,
+               float *g_glideloopROLL, float *g_glideloopPITCH
+               ){
+
+    pc.printf("SDsetup start.\r\n");    
+    
+    FILE *fp;
+    char parameter[30]; //文字列渡す用の配列
+    int SDerrorcount = 0;  //取得できなかった数を返す
+    const char *paramNames[] = { 
+        "KP_ELEVATOR",
+        "KI_ELEVATOR",
+        "KD_ELEVATOR",
+        "KP_RUDDER",
+        "KI_RUDDER",
+        "KD_RUDDER",
+        "RIGHTLOOP_ROLL",
+        "RIGHTLOOP_PITCH",
+        "LEFTLOOP_ROLL",
+        "LEFTLOOP_PITCH",
+        "GOSTRAIGHT_ROLL",
+        "GOSTRAIGHT_PITCH",
+        "TAKEOFF_THR_RATE",
+        "LOOP_THR_RATE",
+        "RIGHTLOOP_ROLL_SHORT",
+        "RIGHTLOOP_PITCH_SHORT",
+        "LEFTLOOP_ROLL_SHORT",
+        "LEFTLOOP_PITCH_SHORT",
+        "AUTOGLIDE_ROLL",
+        "AUTOGLIDE PITCH"        
+    };
+
+    fp = fopen("/sd/option.txt","r");
+    
+    if(fp != NULL){ //開けたら
+        pc.printf("File was openned.\r\n");
+        if(GetParameter(fp,paramNames[0],parameter)) *g_kpELE = atof(parameter);
+        else{                                        *g_kpELE = KP_ELE;
+                                                     SDerrorcount++;
+        }
+        if(GetParameter(fp,paramNames[1],parameter)) *g_kiELE = atof(parameter);
+        else{                                        *g_kiELE = KI_ELE;
+                                                      SDerrorcount++;
+        }
+        if(GetParameter(fp,paramNames[2],parameter)) *g_kdELE = atof(parameter);
+        else{                                        *g_kdELE = KD_ELE;
+                                                     SDerrorcount++;
+        }
+        if(GetParameter(fp,paramNames[3],parameter)) *g_kpRUD = atof(parameter);
+        else{                                        *g_kpRUD = KP_RUD;
+                                                      SDerrorcount++;
+        }
+        if(GetParameter(fp,paramNames[4],parameter)) *g_kiRUD = atof(parameter);
+        else{                                        *g_kiRUD = KI_RUD;
+                                                      SDerrorcount++;
+        }
+        if(GetParameter(fp,paramNames[5],parameter)) *g_kdRUD = atof(parameter);
+        else{                                        *g_kdRUD = KD_RUD;
+                                                      SDerrorcount++;
+        }
+        if(GetParameter(fp,paramNames[6],parameter)) *g_rightloopROLL = atof(parameter);
+        else{                                        *g_rightloopROLL = RIGHT_ROLL;
+                                                      SDerrorcount++;
+        }
+        if(GetParameter(fp,paramNames[7],parameter)) *g_rightloopPITCH = atof(parameter);
+        else{                                        *g_rightloopPITCH = RIGHT_PITCH;
+                                                      SDerrorcount++;
+        }
+        if(GetParameter(fp,paramNames[8],parameter)) *g_leftloopROLL = atof(parameter);
+        else{                                        *g_leftloopROLL = LEFT_ROLL;
+                                                      SDerrorcount++;
+        }
+        if(GetParameter(fp,paramNames[9],parameter)) *g_leftloopPITCH = atof(parameter);
+        else{                                         *g_leftloopPITCH = LEFT_PITCH;
+                                                      SDerrorcount++;
+        }
+        if(GetParameter(fp,paramNames[10],parameter)) *g_gostraightROLL = atof(parameter);
+        else{                                         *g_gostraightROLL = STRAIGHT_ROLL;
+                                                      SDerrorcount++;
+        }
+        if(GetParameter(fp,paramNames[11],parameter)) *g_gostraightPITCH = atof(parameter);
+        else{                                         *g_gostraightPITCH = STRAIGHT_PITCH;
+                                                      SDerrorcount++;
+        }
+        if(GetParameter(fp,paramNames[12],parameter)) *g_takeoffTHR = atof(parameter);
+        else{                                         *g_takeoffTHR = TAKEOFF_THR;
+                                                      SDerrorcount++;
+        }
+        if(GetParameter(fp,paramNames[13],parameter)) *g_loopTHR = atof(parameter);
+        else{                                         *g_loopTHR = LOOP_THR;
+                                                      SDerrorcount++;
+        }
+        if(GetParameter(fp,paramNames[14],parameter)) *g_rightloopROLLshort = atof(parameter);
+        else{                                         *g_rightloopROLLshort = RIGHT_ROLL_SHORT;
+                                                      SDerrorcount++;
+        }
+        if(GetParameter(fp,paramNames[15],parameter)) *g_rightloopPITCHshort = atof(parameter);
+        else{                                         *g_rightloopPITCHshort = RIGHT_PITCH_SHORT;
+                                                      SDerrorcount++;
+        }
+        if(GetParameter(fp,paramNames[16],parameter)) *g_leftloopROLLshort = atof(parameter);
+        else{                                         *g_leftloopROLLshort = LEFT_ROLL_SHORT;
+                                                      SDerrorcount++;
+        }
+        if(GetParameter(fp,paramNames[17],parameter)) *g_leftloopPITCHshort = atof(parameter);
+        else{                                         *g_leftloopPITCHshort = LEFT_PITCH_SHORT;
+                                                      SDerrorcount++;
+        }
+        if(GetParameter(fp,paramNames[18],parameter)) *g_glideloopROLL = atof(parameter);
+        else{                                         *g_glideloopROLL = GLIDE_ROLL;
+                                                      SDerrorcount++;
+        }
+        if(GetParameter(fp,paramNames[19],parameter)) *g_glideloopPITCH = atof(parameter);
+        else{                                         *g_glideloopPITCH = GLIDE_PITCH;
+                                                      SDerrorcount++;
+        }
+        fclose(fp);
+
+    }else{  //ファイルがなかったら
+        pc.printf("fp was null.\r\n");
+        *g_kpELE = KP_ELE;
+        *g_kiELE = KI_ELE;
+        *g_kdELE = KD_ELE;
+        *g_kpRUD = KP_RUD;
+        *g_kiRUD = KI_RUD;
+        *g_kdRUD = KD_RUD;
+        *g_rightloopROLL = RIGHT_ROLL;
+        *g_rightloopPITCH = RIGHT_PITCH;
+        *g_leftloopROLL = LEFT_ROLL;
+        *g_leftloopPITCH = LEFT_PITCH;
+        *g_gostraightROLL = STRAIGHT_ROLL;
+        *g_gostraightPITCH = STRAIGHT_PITCH;
+        *g_takeoffTHR = TAKEOFF_THR;
+        *g_loopTHR = LOOP_THR;
+        SDerrorcount = -1;
+    }
+    pc.printf("SDsetup finished.\r\n");
+    if(SDerrorcount == 0)  pc.printf("setting option is success\r\n");
+    else if(SDerrorcount == -1) pc.printf("ERROR 1. cannot open option\r\n");
+    else if(SDerrorcount > 0)  pc.printf("ERROR 2. reading parameter is failed[%d]\r\n",SDerrorcount); 
+    
+    pc.printf("kpELE = %f, kiELE = %f, kdELE = %f\r\n", *g_kpRUD, *g_kiRUD, *g_kdRUD);
+    pc.printf("kpRUD = %f, kiRUD = %f, kdRUD = %f\r\n", *g_kpELE, *g_kiELE, *g_kdELE);
+    pc.printf("rightloopROLL = %f, rightloopPITCH = %f\r\n", *g_rightloopROLL, *g_rightloopPITCH);
+    pc.printf("leftloopROLL = %f, g_leftloopPITCH =  %f\r\n", *g_leftloopROLL, *g_leftloopPITCH);
+    pc.printf("gostraightROLL = %f, g_gostraightPITCH = %f\r\n", *g_gostraightROLL, *g_gostraightPITCH);
+    pc.printf("g_takeoffTHR = %f, g_loopTHR = %f\r\n", *g_takeoffTHR, *g_loopTHR);
+    pc.printf("rightloopROLLshort = %f, rightloopPITCHshort = %f\r\n", *g_rightloopROLLshort, *g_rightloopPITCHshort);
+    pc.printf("leftloopROLLshort = %f, g_leftloopPITCHshort =  %f\r\n", *g_leftloopROLLshort, *g_leftloopPITCHshort);
+    pc.printf("glideROLL = %f, glidePITCH = %f\r\n", *g_glideloopROLL, *g_glideloopPITCH);
+    
+    return SDerrorcount;
+}                  
+
+void CalculateControlValue(float targetAngle[3], float controlValue[3]){
+    static int t_last;
+    int t_now;
+    float dt;
+
+    t_now = t.read_us();
+    dt = (float)((t_now - t_last)/1000000.0f) ;
+    t_last = t_now;
+
+    controlValue[ROLL] = pid_RUD.calcPID(nowAngle[ROLL], targetAngle[ROLL], dt);    
+    controlValue[PITCH] = pid_ELE.calcPID(nowAngle[PITCH], targetAngle[PITCH], dt);
+}
+
+void UpdateAutoPWM(float controlValue[3]){    
+    int16_t addpwm[2]; //-500~500
+    addpwm[PITCH] = (float)GAIN_CONTROLVALUE_TO_PWM * controlValue[PITCH];    //センサ:機首下げ正    レバー:機首上げ正
+    addpwm[ROLL] = (float)GAIN_CONTROLVALUE_TO_PWM * controlValue[ROLL];           //センサ:右回転正(8月13日時点;左回転が正!)     レバー:右回転正
+    
+    autopwm[ELE] = trimpwm[ELE] + reverce[ELE] * addpwm[PITCH];
+    autopwm[RUD] = trimpwm[RUD] + reverce[RUD] * addpwm[ROLL];
+    //autopwm[THR] = oldTHR;
+
+    autopwm[ELE] = ThresholdMaxMin(autopwm[ELE], maxpwm[ELE], minpwm[ELE]);
+    autopwm[RUD] = ThresholdMaxMin(autopwm[RUD], maxpwm[RUD], minpwm[RUD]);
+}
+
+inline float CalcRatio(float value, float trim, float limit){
+    return  (value - trim) / (limit - trim);
+}
+
+bool CheckSW_Up(Channel ch){
+    if(SWITCH_CHECK < sbus.manualpwm[ch]){
+        return true;
+    }else{
+        return false;
+    }
+}
+
+int16_t ThresholdMaxMin(int16_t value, int16_t max, int16_t min){
+    if(value > max) return max;
+    if(value < min) return min;
+    return value;
+}
+
+inline int16_t SetTHRinRatio(float ratio){
+    return minpwm[THR] + (int16_t)(2 * lengthdivpwm * ratio);
+}
+
+/*---SBUS割り込み処理---*/
+
+//udate_Inputで抽出したpwmデータを整形して各変数に代入する。(マニュアルモード)
+//各stabiGylo関数で算出したpwmを各変数に代入する(自動モード)
+void Update_PWM()
+{    
+    static int16_t pwm[6];
+    static int16_t temppwm[6]={trimpwm[0],trimpwm[1],trimpwm[2],trimpwm[3],trimpwm[4],trimpwm[5]};
+    if(sbus.flg_ch_update == true){
+        switch(output_status){    //マニュアルモード,自動モード,自動着陸もモードを切替
+            case Manual: 
+                for(uint8_t i=0;i<6;i++){
+                    pwm[i] = sbus.manualpwm[i];
+                    pc.printf("%d ,",pwm[i]);
+                }
+                oldTHR = sbus.manualpwm[THR];
+                //pc.printf("update_manual\r\n");
+                break;
+        
+            case Auto:
+                pwm[AIL_R] = autopwm[AIL_R];               //sbus.manualpwm[AIL];
+                pwm[ELE] = autopwm[ELE];
+                pwm[THR] = autopwm[THR];
+                pwm[RUD] = autopwm[RUD];
+                pwm[DROP] = autopwm[DROP];
+                pwm[AIL_L] = autopwm[AIL_L];
+                //pc.printf("update_auto\r\n");
+                break;
+                
+            default:
+                for(uint8_t i=0;i<6;i++){
+                    pwm[i] = sbus.manualpwm[i];
+                } //pc.printf("update_manual\r\n");
+                break;
+        }
+        for(uint8_t i=0;i<6;i++){
+        if(pwm[i]<1000 || pwm[i]>2000) pwm[i]=temppwm[i];
+        temppwm[i]=pwm[i];
+        }
+    }else{
+        pc.printf("0\r\n");
+    }
+    sbus.flg_ch_update = false;   
+    Output_PWM(pwm);  
+}
+
+
+//pwmをサーボに出力。
+void Output_PWM(int16_t pwm[5])
+{
+    servo1.pulsewidth_us(pwm[0]);
+    servo2.pulsewidth_us(pwm[1]);
+    servo3.pulsewidth_us(pwm[2]);
+    servo4.pulsewidth_us(pwm[3]);
+    servo5.pulsewidth_us(pwm[4]);
+    servo6.pulsewidth_us(pwm[5]);
+
+}
+
+void ResetTrim(){
+    for(uint8_t i=0; i<6; i++){            //i=4から書き換え_投下サーボは入ってない模様
+        trimpwm[i] = sbus.manualpwm[i];
+    }
+    pc.printf("reset PWM trim\r\n");
+}
+
+
+void SensingMPU(){
+    //static int16_t deltaT = 0, t_start = 0;
+    //t_start = t.read_us();
+    
+    float rpy[3] = {0}, oldrpy[3] = {0};
+    static uint16_t count_changeRPY = 0;
+    static bool flg_checkoutlier = false;
+    NVIC_DisableIRQ(USART1_IRQn);
+    NVIC_DisableIRQ(USART2_IRQn);
+    NVIC_DisableIRQ(TIM5_IRQn);
+    NVIC_DisableIRQ(EXTI0_IRQn);
+    NVIC_DisableIRQ(EXTI9_5_IRQn);
+
+    mpu6050.getRollPitchYaw_Skipper(rpy);
+ 
+    NVIC_EnableIRQ(USART1_IRQn);
+    NVIC_EnableIRQ(USART2_IRQn);
+    NVIC_EnableIRQ(TIM5_IRQn);
+    NVIC_EnableIRQ(EXTI0_IRQn);
+    NVIC_EnableIRQ(EXTI9_5_IRQn);
+    
+    
+    //外れ値対策
+    for(uint8_t i=0; i<3; i++) rpy[i] *= 180.0f/PI;
+    rpy[ROLL] -= FirstROLL;
+    rpy[PITCH] -= FirstPITCH;
+    rpy[YAW] -= FirstYAW;
+    
+    for(uint8_t i=0; i<3; i++) {if(rpy[i] < nowAngle[i]-10 || rpy[i] > nowAngle[i]+10) {flg_checkoutlier = true;}}
+    if(!flg_checkoutlier || count_changeRPY >= 2){
+        for(uint8_t i=0; i<3; i++){
+            nowAngle[i] = (rpy[i] + nowAngle[i])/2.0f;  //2つの移動平均
+        }
+        count_changeRPY = 0;
+    }else   count_changeRPY++;
+    flg_checkoutlier = false;
+    
+}
+
+float TranslateNewYaw(float beforeYaw,  float newzeroYaw){
+    float newYaw = beforeYaw - newzeroYaw;
+    
+    if(newYaw<-180.0f) newYaw += 360.0f;
+    else if(newYaw>180.0f) newYaw -= 360.0f;
+    return newYaw;
+}
+
+
+void getSF_Serial(){
+    
+        static char SFbuf[16];
+        static int bufcounter=0;
+        
+        SFbuf[bufcounter]=pc.getc();
+        if(SFbuf[0]=='S'&&bufcounter<5) bufcounter++;
+            
+        if(bufcounter==5 && SFbuf[4]=='F'){
+            g_landingcommand = SFbuf[1];
+            if(g_landingcommand=='Y')g_SerialTargetYAW = ConvertByteintoFloat(SFbuf[2], SFbuf[3]);
+            bufcounter = 0;
+            memset(SFbuf, 0, strlen(SFbuf));
+            pc.printf("command = %c, commandYAW = %f\r\n", g_landingcommand, g_SerialTargetYAW); 
+        }
+            else if(bufcounter>=5 && g_buf[4]!='F'){
+                pc.printf("Communication Falsed.\r\n");
+                bufcounter = 0;
+            }
+    }
+    
+float ConvertByteintoFloat(char high, char low){
+
+        //int16_t intvalue = (int16_t)high*256 + (int16_t)low;
+        int16_t intvalue = (int16_t)(((int16_t)high << 8) | low);  // Turn the MSB and LSB into a signed 16-bit value
+        float floatvalue = (float)intvalue;
+        return floatvalue;
+}
+
+
+//超音波割り込み
+void UpdateDist(){
+    g_distance = usensor.get_dist_cm();
+    usensor.start();
+}
+
+//8の字旋回
+void UpdateTargetAngle_Moebius(float targetAngle[3]){
+    static uint8_t RotateCounter=0;
+    static bool flg_setInStartAuto = false;
+    static float FirstYAW_Moebius = 0.0;
+    float newYaw_Moebius;
+
+    if(!flg_setInStartAuto && CheckSW_Up(Ch7)){
+        FirstYAW_Moebius = nowAngle[YAW];
+        RotateCounter = 0;
+        flg_setInStartAuto = true;
+    }else if(!CheckSW_Up(Ch7)){
+        flg_setInStartAuto = false;
+        led2 = 0;
+    }
+    
+    newYaw_Moebius = TranslateNewYaw(nowAngle[YAW], FirstYAW_Moebius);
+
+    if(RotateCounter == 0 && newYaw_Moebius >90.0 && newYaw_Moebius < 180.0)    {RotateCounter++; led2 = 1; pc.printf("Rotate 90\r\n");}
+    if(RotateCounter == 1 && newYaw_Moebius >-180.0 && newYaw_Moebius < -90.0)  {RotateCounter++; led2 = 0; pc.printf("Rotate 180\r\n");}
+    if(RotateCounter == 2 && newYaw_Moebius >-90.0 && newYaw_Moebius < 10.0f)   {RotateCounter++; led2 = 1; pc.printf("Rotate 270\r\n");}
+    if(RotateCounter == 3 && newYaw_Moebius >20.0 && newYaw_Moebius < 180.0f)     {RotateCounter++; led2 = 0; pc.printf("Change Rotate direction\r\n");}
+
+
+    if(RotateCounter <= 3) UpdateTargetAngle_Rightloop_short(targetAngle);    
+    else UpdateTargetAngle_Leftloop_short(targetAngle);   //左旋回
+
+}
+
+//自動滑空
+void UpdateTargetAngle_Glide(float targetAngle[3]){
+    static int THRcount = 0;
+    static int t_start = 0;
+    static bool flg_tstart = false;
+    int t_diff = 0;
+    
+    targetAngle[ROLL] = g_glideloopROLL;
+    targetAngle[PITCH] = g_glideloopPITCH;
+    
+    //時間計測開始設定
+    if(!flg_tstart && CheckSW_Up(Ch7)){
+        t_start = t.read();
+        flg_tstart = true;
+        pc.printf("timer start\r\n");
+    }else if(flg_tstart && !CheckSW_Up(Ch7)){
+        t_start = 0;
+        flg_tstart = false;
+    }
+
+    //フラグが偽であれば計測は行わない    
+    if(flg_tstart){
+        t_diff = t.read() - t_start;
+        //一定高度or15秒でled点灯
+        if((g_distance<200 && g_distance>0) || t_diff > 15){
+            led2 = 1;
+            //pc.printf("Call [Stop!] calling!\r\n");
+        }
+    }else{
+        t_diff = 0;
+        led2 = 0;
+    }
+    
+    if(t_diff > 18){
+        autopwm[THR] = SetTHRinRatio(0.5);
+    }else{
+        if(g_distance<150 && g_distance>0 ){
+            THRcount++;
+            if(THRcount>5){
+                autopwm[THR] = SetTHRinRatio(0.5);
+                //pc.printf("throttle ON\r\n");
+            }
+        }else{
+            autopwm[THR] = 1180;
+            THRcount = 0;
+        }
+    }
+}
+
+//離陸-投下-着陸一連
+void Take_off_and_landing(float targetAngle[3]){
+    if(!CheckSW_Up(Ch7)) bombing_mode = Takeoff;
+    
+    switch(bombing_mode){
+        case Takeoff:
+            static bool flg_setFirstYaw = false;
+            static int TakeoffCount = 0;
+
+            if(!flg_setFirstYaw && CheckSW_Up(Ch7)){
+                FirstYAW = nowAngle[YAW];
+                flg_setFirstYaw = true;
+            }else if(flg_setFirstYaw && !CheckSW_Up(Ch7)){
+                flg_setFirstYaw = false;
+            }
+            
+            UpdateTargetAngle_Takeoff(targetAngle);
+            
+            if(g_distance>150) TakeoffCount++;
+            else TakeoffCount = 0;
+            if(TakeoffCount>5){
+                autopwm[THR] = 1180+320*2*0.5;
+                pc.printf("Now go to Approach mode!!");
+                bombing_mode = Approach;
+            }
+            break;
+        /*    
+        case Chicken:    
+            break;
+        */    
+        case Transition:
+            static int ApproachCount = 0;
+            targetAngle[YAW]=180.0;
+            int Judge = Rotate(targetAngle, g_SerialTargetYAW);
+            
+            if(Judge==0) ApproachCount++;
+            if(ApproachCount>5) bombing_mode = Approach;
+            break;
+            
+        case Approach:
+            UpdateTargetAngle_Approach(targetAngle);
+            break;
+            
+        default:
+            bombing_mode = Takeoff;
+            break;    
+    }
+}
+
+//離陸モード
+void UpdateTargetAngle_Takeoff(float targetAngle[3]){
+    //pc.printf("%d \r\n",g_distance);
+    targetAngle[ROLL] = g_gostraightROLL;
+    targetAngle[PITCH] = g_loopTHR;
+    autopwm[THR] = SetTHRinRatio(g_takeoffTHR); //0.7;スロットルの割合
+}
+
+//ヨーを目標値にして許容角度になるまで水平旋回
+int Rotate(float targetAngle[3], float TargetYAW){
+    float diffYaw = TranslateNewYaw(TargetYAW, nowAngle[YAW]);
+
+    if(diffYaw > LIMIT_STRAIGHT_YAW){
+        /*
+        if(diffYaw > THRESHOLD_TURNINGRADIUS_YAW) UpdateTargetAngle_Rightloop_short(targetAngle);
+        else UpdateTargetAngle_Rightloop(targetAngle);
+        */
+        UpdateTargetAngle_Rightloop_short(targetAngle);
+        return 1;
+    }else if(diffYaw < -LIMIT_STRAIGHT_YAW){
+        UpdateTargetAngle_Leftloop_short(targetAngle);
+        /*
+        if(diffYaw < -THRESHOLD_TURNINGRADIUS_YAW) UpdateTargetAngle_Leftloop_short(targetAngle);
+        else UpdateTargetAngle_Leftloop(targetAngle);
+        */
+        return 1;
+    }else{
+        UpdateTargetAngle_GoStraight(targetAngle);
+        return 0;
+    }
+}
+
+//チキラー投下
+void Chicken_Drop(){
+    if(CheckSW_Up(Ch7)){
+        autopwm[DROP] = 1512;
+        pc.printf("Bombed!\r\n");
+        RerurnChickenServo1.attach(&ReturnChickenServo1, 3);
+        //operation_mode = Approach;
+        //buzzer = 0;
+        pc.printf("Goto LeftLoop mode\r\n");
+    }
+}
+
+void ReturnChickenServo1(){
+    autopwm[DROP] = 1344;
+    pc.printf("first reverse\r\n");
+    RerurnChickenServo2.attach(&ReturnChickenServo2, 1);
+}
+
+void ReturnChickenServo2(){
+    autopwm[DROP] = 1392;
+    pc.printf("second reverse\r\n");
+}
+
+//着陸モード(PCからの指令に従う)
+void UpdateTargetAngle_Approach(float targetAngle[3]){
+    pc.putc(g_buf[0]);
+    switch(g_buf[0]){
+        case 'R':   //右旋回セヨ
+            UpdateTargetAngle_Rightloop(targetAngle);
+            break;
+            
+        case 'L':   //左旋回セヨ
+            UpdateTargetAngle_Leftloop(targetAngle);
+            break;
+            
+        case 'G':   //直進セヨ
+            UpdateTargetAngle_GoStraight(targetAngle);
+            break;
+        
+        case 'Y':   //指定ノヨー方向ニ移動セヨ
+            Rotate(targetAngle, g_SerialTargetYAW);
+            break;
+        
+        case 'B':   //ブザーヲ鳴ラセ
+            //buzzer = 1;
+            break;
+            
+        case 'D':   //物資ヲ落トセ
+            Chicken_Drop();
+            break;
+                    
+        case 'C':   //停止セヨ
+            targetAngle[ROLL] = 0.0;
+            targetAngle[PITCH] = -3.0;
+            autopwm[THR] = minpwm[THR];
+            break;
+    }
+}
+
+void checkHeight(float targetAngle[3]){
+    
+    static int targetHeight = 200; 
+    
+    if(g_distance < targetHeight + ALLOWHEIGHT){
+        UpdateTargetAngle_NoseUP(targetAngle);
+        if(CheckSW_Up(Ch7)) led2 = 1;
+    }
+    else if(g_distance > targetHeight - ALLOWHEIGHT){
+        UpdateTargetAngle_NoseDOWN(targetAngle);
+        if(CheckSW_Up(Ch7)) led2 = 1;
+    }
+    else led2=0;
+}
+
+void UpdateTargetAngle_NoseUP(float targetAngle[3]){
+    
+    //targetAngle[PITCH] += 2.0f;
+    //if(nowAngle[PITCH]<targetAngle[PITCH]) autopwm[THR] = SetTHRinRatio(0.6);
+    autopwm[THR] = SetTHRinRatio(g_loopTHR+0.05);
+    //pc.printf("nose UP");
+}
+
+void UpdateTargetAngle_NoseDOWN(float targetAngle[3]){
+    
+    //targetAngle[PITCH] -= 2.0f;
+    autopwm[THR] = SetTHRinRatio(g_loopTHR-0.05);
+    //pc.printf("nose DOWN");
+}
+
+//直進
+void UpdateTargetAngle_GoStraight(float targetAngle[3]){
+
+    targetAngle[ROLL] = g_gostraightROLL;
+    targetAngle[PITCH] = g_gostraightPITCH;
+    autopwm[THR] = SetTHRinRatio(g_loopTHR);
+    
+    //pc.printf("Roll = %f, PITCH = %f, THR = %d \r\n", targetAngle[ROLL], targetAngle[PITCH], autopwm[THR]);
+}
+
+//右旋回
+void UpdateTargetAngle_Rightloop(float targetAngle[3]){ //右旋回
+
+    targetAngle[ROLL] = g_rightloopROLL;
+    targetAngle[PITCH] = g_rightloopPITCH ;
+    autopwm[THR] = SetTHRinRatio(g_loopTHR);
+    //checkHeight(targetAngle);
+    //pc.printf("Roll = %f, PITCH = %f, THR = %d \r\n", targetAngle[ROLL], targetAngle[PITCH], autopwm[THR]);
+}
+
+void UpdateTargetAngle_Rightloop_short(float targetAngle[3]){ //右旋回
+
+    targetAngle[ROLL] = g_rightloopROLLshort;
+    targetAngle[PITCH] = g_rightloopPITCHshort;
+    autopwm[THR] = SetTHRinRatio(g_loopTHR);
+    
+    
+    //pc.printf("Roll = %f, PITCH = %f, THR = %d \r\n", targetAngle[ROLL], targetAngle[PITCH], autopwm[THR]);
+}
+
+//左旋回
+void UpdateTargetAngle_Leftloop(float targetAngle[3]){
+    
+    targetAngle[ROLL] = g_leftloopROLL;
+    targetAngle[PITCH] = g_leftloopPITCH;
+    autopwm[THR] = SetTHRinRatio(g_loopTHR);
+    //checkHeight(targetAngle);
+
+    //printf("Roll = %f, PITCH = %f, THR = %d \r\n", targetAngle[ROLL], targetAngle[PITCH], autopwm[THR]);
+}
+
+void UpdateTargetAngle_Leftloop_short(float targetAngle[3]){
+    
+    targetAngle[ROLL] = g_leftloopROLLshort;
+    targetAngle[PITCH] = g_leftloopPITCHshort;
+    autopwm[THR] = SetTHRinRatio(g_loopTHR);
+    
+    //pc.printf("Roll = %f, PITCH = %f, THR = %d \r\n", targetAngle[ROLL], targetAngle[PITCH], autopwm[THR]);
+}
+
+//デバッグ用
+void DebugPrint(){    
+    /*
+    static int16_t deltaT = 0, t_start = 0;
+    deltaT = t.read_u2s() - t_start;
+    pc.printf("t:%d us, ",deltaT);
+    pc.printf("\r\n");
+    t_start = t.read_us();
+    */
+    //for(uint8_t i=0; i<8; i++) pc.printf("%d ",sbus.manualpwm[i]);
+    //for(uint8_t i=1; i<4; i++) pc.printf("%d ",sbus.manualpwm[i]);
+    //pc.printf("\r\n");
+    for(uint8_t i=0; i<3; i++) pc.printf("%3.2f\t",nowAngle[i]);
+    //for(uint8_t i=0; i<2; i++) pc.printf("%3.2f\t",nowAngle[i]); //ロール、ピッチのみ 小数点以下2ケタ
+    //pc.printf("%d\t",autopwm[ELE]);  pc.printf("%d\t",autopwm[RUD]);
+    //pc.printf("%d",g_distance);
+
+    //pc.printf("Mode: %c: ",g_buf[0]);
+    //if(g_buf[0] == 'Y') pc.printf(" %3.1f",g_SerialTargetYAW);
+    pc.printf("\r\n");
+}
\ No newline at end of file