// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*- /* This program 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. This program 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 this program. If not, see . */ /* * AP_MotorsQuad.cpp - ArduCopter motors library * Code by RandyMackay. DIYDrones.com * */ #include "AP_MotorsQuad.h" // setup_motors - configures the motors for a quad void AP_MotorsQuad::setup_motors() { // call parent AP_MotorsMatrix::setup_motors(); // hard coded config for supported frames if( _flags.frame_orientation == AP_MOTORS_PLUS_FRAME ) { // plus frame set-up add_motor(AP_MOTORS_MOT_1, 90, AP_MOTORS_MATRIX_YAW_FACTOR_CCW, 2); add_motor(AP_MOTORS_MOT_2, -90, AP_MOTORS_MATRIX_YAW_FACTOR_CCW, 4); add_motor(AP_MOTORS_MOT_3, 0, AP_MOTORS_MATRIX_YAW_FACTOR_CW, 1); add_motor(AP_MOTORS_MOT_4, 180, AP_MOTORS_MATRIX_YAW_FACTOR_CW, 3); }else if( _flags.frame_orientation == AP_MOTORS_V_FRAME ) { // V frame set-up add_motor(AP_MOTORS_MOT_1, 45, 0.7981, 1); add_motor(AP_MOTORS_MOT_2, -135, 1.0000, 3); add_motor(AP_MOTORS_MOT_3, -45, -0.7981, 4); add_motor(AP_MOTORS_MOT_4, 135, -1.0000, 2); }else if( _flags.frame_orientation == AP_MOTORS_H_FRAME ) { // H frame set-up - same as X but motors spin in opposite directiSons add_motor(AP_MOTORS_MOT_1, 45, AP_MOTORS_MATRIX_YAW_FACTOR_CW, 1); add_motor(AP_MOTORS_MOT_2, -135, AP_MOTORS_MATRIX_YAW_FACTOR_CW, 3); add_motor(AP_MOTORS_MOT_3, -45, AP_MOTORS_MATRIX_YAW_FACTOR_CCW, 4); add_motor(AP_MOTORS_MOT_4, 135, AP_MOTORS_MATRIX_YAW_FACTOR_CCW, 2); } else if (_flags.frame_orientation == AP_MOTORS_VTAIL_FRAME) { /* Lynxmotion Hunter Vtail 400/500 Roll control comes only from the front motors, Yaw control only from the rear motors roll factor is measured by the angle perpendicular to that of the prop arm to the roll axis (x) pitch factor is measured by the angle perpendicular to the prop arm to the pitch axis (y) assumptions: 20 20 \ / 3_____________1 \ / | \ / | 40 \/ 40 20 | 20 Tail / \ 2 4 All angles measured from their closest axis Note: if we want the front motors to help with yaw, motors 1's yaw factor should be changed to sin(radians(40)). Where "40" is the vtail angle motors 3's yaw factor should be changed to -sin(radians(40)) */ // front right: 70 degrees right of roll axis, 20 degrees up of pitch axis, no yaw add_motor_raw(AP_MOTORS_MOT_1, cosf(radians(160)), cosf(radians(-70)), 0, 1); // back left: no roll, 70 degrees down of pitch axis, full yaw add_motor_raw(AP_MOTORS_MOT_2, 0, cosf(radians(160)), AP_MOTORS_MATRIX_YAW_FACTOR_CCW, 3); // front left: 70 degrees left of roll axis, 20 degrees up of pitch axis, no yaw add_motor_raw(AP_MOTORS_MOT_3, cosf(radians(20)), cosf(radians(70)), 0, 4); // back right: no roll, 70 degrees down of pitch axis, full yaw add_motor_raw(AP_MOTORS_MOT_4, 0, cosf(radians(-160)), AP_MOTORS_MATRIX_YAW_FACTOR_CW, 2); }else{ // X frame set-up add_motor(AP_MOTORS_MOT_1, 45, AP_MOTORS_MATRIX_YAW_FACTOR_CCW, 1); add_motor(AP_MOTORS_MOT_2, -135, AP_MOTORS_MATRIX_YAW_FACTOR_CCW, 3); add_motor(AP_MOTORS_MOT_3, -45, AP_MOTORS_MATRIX_YAW_FACTOR_CW, 4); add_motor(AP_MOTORS_MOT_4, 135, AP_MOTORS_MATRIX_YAW_FACTOR_CW, 2); } }