// ------------------------------------------------------------------ // Z-WING2025 PIC12F1572 (C)2025.12.31 inakakoubouKANAI // FLP2 // + :Vcd Vss: - // ELE IN :RA5 RA0: IN RUD // MAIN IN :RA4 RA1: OUT PWM1 → Servo // GYR3 RUD IN :RA3 RA2: IN GYR2 ELE or AIL // ------------------------------------------------------------------ #include #include #define _XTAL_FREQ 16000000 //delayマクロ用 16MHz // CONFIG #pragma config FOSC = INTOSC, WDTE = OFF, PWRTE = ON, MCLRE = OFF, CP = OFF, BOREN = ON, LVP = OFF // --- 変数宣言 (int16_tに統一) --- int16_t RUDSENTER, RUD; int16_t GYR2SENTER, GYR2; int16_t GYR3SENTER, GYR3; int16_t MAINSENTER, MAIN0; int16_t ELESENTER, ELE; int16_t GS, G0, G1, G2, G3,GELE0,GELE1; int16_t h = 1; // --- PDI制御用変数 --- int16_t gyro2_err_prev = 0, gyro3_err_prev = 0; int32_t gyro2_integral = 0, gyro3_integral = 0; // --- PDIゲイン(要現場調整) --- int16_t Kp2 = 0, Ki2 = 0, Kd2 = 1; // GYR2: エレベータ(またはエルロンピッチ軸) int16_t Kp3 = 0, Ki3 = 0, Kd3 = 1; // GYR3: ラダー(ヨー軸) //---------------- 初期化 ---------------- void p_initialize() { OSCCON = 0b01111000; //16MHz ANSELA = 0b00000000; TRISA = 0b1111101; // RA1出力 WPUA = 0b1111101; OPTION_REGbits.nWPUEN = 0; INTCON = 0x00; LATA = 0b00000000; } void PWM_Initialize(void) { OSCCON = 0x7A; while(!OSCSTATbits.HFIOFS); } void out_Initialize(void) { PWM1CLKCON = 0b00000000; PWM1TMR = 0; PWM1CLKCON |= (0b100 << 3); PWM1CON = 0b11000000; PWM1DCH = (6000 >> 8) & 0xFF; PWM1DCL = 6000 & 0xFF; PWM1PHH = 0; PWM1PHL = 0; PWM1LDCONbits.LDA = 1; while(PWM1LDCONbits.LDA == 1); } // --- 範囲制限処理 --- int16_t clip_range(int16_t a, int16_t min, int16_t max) { if (a < min) return min; if (a > max) return max; return a; } // --- PWM出力 --- void out_PWM(int16_t pulse) { PWM1DCH = (pulse >> 8) & 0xFF; PWM1DCL = pulse & 0xFF; PWM1PHH = 0; PWM1PHL = 0; PWM1LDCONbits.LDA = 1; while(PWM1LDCONbits.LDA == 1); } // --- 汎用PDI演算 --- int16_t pdi_control(int16_t gyro, int16_t center, int16_t *prev, int32_t *integ, int16_t Kp, int16_t Ki, int16_t Kd) { int16_t err = gyro - center; int16_t p = err * Kp; int16_t d = (err - *prev) * Kd; *prev = err; *integ += err; if (*integ > 2000) *integ = 2000; if (*integ < -2000) *integ = -2000; int16_t i = (int16_t)((*integ * Ki) >> 6); return (p + i + d) >> 2; } // D制御のみに特化したシンプルな関数例 int16_t d_control_only(int16_t gyro, int16_t center, int16_t *prev, int16_t Kd) { int16_t err = gyro - center; int16_t d = (err - *prev) * Kd; *prev = err; //return d >> 2; // スケーリング(必要に応じて調整) return d ; } //■■■■■■■■■■■■■■■ Z-WING制御用に合成 ■■■■■■■■■■■■■■ void out_steering() { //---GYR3によるラダーポイントの移動 RUD=RUD+GYR3-GYR3SENTER; //--- ヒステリシス状態 --- if (ELE > (ELESENTER + 360)) { h = 2; } else if (ELE < (ELESENTER + 350)) { h = 1; } // --- ラダー応答モード別処理 --- if (h > 1) { //----反転----- if (RUDSENTER > RUD) { G0 = RUDSENTER - RUD; G2 = G0 >> 2; GS = MAIN0 - G2; } else { G0 = RUD - RUDSENTER; G2 = G0 >> 2; GS = MAIN0 + G2; } } else { //---通常---- if (RUDSENTER > RUD) { G0 = RUDSENTER - RUD; G1 = G0 >> 1; GS = MAIN0 - G1; } else { G0 = RUD - RUDSENTER; G2 = G0 >> 2; GS = MAIN0 - G2; } } //--- 送信機からのピッチコントロール --- GELE0 = ELESENTER >> 2; GELE1 = ELE >> 2; GS = GS + GELE0 - GELE1; //--- GYR2/GYR3 双方にPDI制御 --- //int16_t pitch_offset = pdi_control(GYR2, GYR2SENTER, &gyro2_err_prev, &gyro2_integral, Kp2, Ki2, Kd2); //int16_t yaw_offset = pdi_control(GYR3, GYR3SENTER, &gyro3_err_prev, &gyro3_integral, Kp3, Ki3, Kd3); int16_t pitch_offset = d_control_only(GYR3, GYR3SENTER, &gyro3_err_prev, Kd3); int16_t yaw_offset = d_control_only(GYR3, GYR3SENTER, &gyro3_err_prev, Kd3); //---GYR21でピッチコントロール GS+=GYR2-GYR2SENTER-pitch_offset; //---GYR3でヨーコントロール GYRから右舵が来たら上げる if((GYR3-yaw_offset)