mirror of https://github.com/ArduPilot/ardupilot
minor cosmetics
git-svn-id: https://arducopter.googlecode.com/svn/trunk@2846 f9c3cf11-9bcb-44bc-f272-b75c42450872
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c22ebd22b4
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@ -8,19 +8,16 @@ void init_camera()
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g.rc_camera_pitch.radio_min = 1000;
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g.rc_camera_pitch.radio_trim = 1500;
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g.rc_camera_pitch.radio_max = 2000;
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g.rc_camera_pitch.set_reverse(g.cam_pitch_reverse);
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g.rc_camera_roll.set_angle(4500);
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g.rc_camera_roll.radio_min = 1000;
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g.rc_camera_roll.radio_trim = 1500;
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g.rc_camera_roll.radio_max = 2000;
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g.rc_camera_roll.set_reverse(g.cam_roll_reverse);
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}
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void
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camera_stabilization()
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{
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// PITCH
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// -----
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// allow control mixing
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@ -201,8 +201,8 @@ void mavlink_send_message(mavlink_channel_t chan, uint8_t id, uint32_t param, ui
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motor_out[2],
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motor_out[3],
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motor_out[4],
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motor_out[6],
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motor_out[7],
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motor_out[8],
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0);
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break;
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}
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@ -104,8 +104,6 @@ public:
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k_param_throttle_cruise,
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k_param_flight_modes,
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k_param_esc_calibrate,
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k_param_cam_pitch_reverse,
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k_param_cam_roll_reverse,
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#if FRAME_CONFIG == HELI_FRAME
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@ -242,9 +240,6 @@ public:
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RC_Channel rc_camera_pitch;
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RC_Channel rc_camera_roll;
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AP_Int8 cam_pitch_reverse;
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AP_Int8 cam_roll_reverse;
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// PID controllers
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PID pid_rate_roll;
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PID pid_rate_pitch;
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@ -330,12 +325,8 @@ public:
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rc_6 (k_param_rc_6, PSTR("RC6_")),
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rc_7 (k_param_rc_7, PSTR("RC7_")),
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rc_8 (k_param_rc_8, PSTR("RC8_")),
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rc_camera_pitch (k_param_rc_9, NULL),
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rc_camera_roll (k_param_rc_10, NULL),
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cam_pitch_reverse (0, k_param_cam_pitch_reverse, PSTR("CAM_P_REV")),
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cam_roll_reverse (0, k_param_cam_roll_reverse, PSTR("CAM_R_REV")),
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rc_camera_pitch (k_param_rc_9, PSTR("RC_CP_")),
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rc_camera_roll (k_param_rc_10, PSTR("RC_CR_")),
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// PID controller group key name initial P initial I initial D initial imax
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//--------------------------------------------------------------------------------------------------------------------------------------------------------------------
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@ -14,6 +14,7 @@ static int8_t test_imu(uint8_t argc, const Menu::arg *argv);
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//static int8_t test_omega(uint8_t argc, const Menu::arg *argv);
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static int8_t test_battery(uint8_t argc, const Menu::arg *argv);
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//static int8_t test_wp_nav(uint8_t argc, const Menu::arg *argv);
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//static int8_t test_reverse(uint8_t argc, const Menu::arg *argv);
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static int8_t test_tuning(uint8_t argc, const Menu::arg *argv);
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static int8_t test_current(uint8_t argc, const Menu::arg *argv);
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static int8_t test_relay(uint8_t argc, const Menu::arg *argv);
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@ -72,6 +73,7 @@ const struct Menu::command test_menu_commands[] PROGMEM = {
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{"eedump", test_eedump},
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{"rawgps", test_rawgps},
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{"mission", test_mission},
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//{"reverse", test_reverse},
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//{"wp", test_wp_nav},
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};
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@ -81,7 +83,7 @@ MENU(test_menu, "test", test_menu_commands);
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int8_t
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test_mode(uint8_t argc, const Menu::arg *argv)
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{
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Serial.printf_P(PSTR("Test Mode\n\n"));
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//Serial.printf_P(PSTR("Test Mode\n\n"));
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test_menu.run();
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}
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@ -899,6 +901,45 @@ test_mag(uint8_t argc, const Menu::arg *argv)
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return (0);
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}
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}
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/*
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static int8_t
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test_reverse(uint8_t argc, const Menu::arg *argv)
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{
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print_hit_enter();
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delay(1000);
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while(1){
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delay(20);
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// Filters radio input - adjust filters in the radio.pde file
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// ----------------------------------------------------------
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g.rc_4.set_reverse(0);
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g.rc_4.set_pwm(APM_RC.InputCh(CH_4));
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g.rc_4.servo_out = g.rc_4.control_in;
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g.rc_4.calc_pwm();
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Serial.printf_P(PSTR("PWM:%d input: %d\toutput%d "),
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APM_RC.InputCh(CH_4),
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g.rc_4.control_in,
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g.rc_4.radio_out);
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APM_RC.OutputCh(CH_6, g.rc_4.radio_out);
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g.rc_4.set_reverse(1);
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g.rc_4.set_pwm(APM_RC.InputCh(CH_4));
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g.rc_4.servo_out = g.rc_4.control_in;
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g.rc_4.calc_pwm();
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Serial.printf_P(PSTR("\trev input: %d\toutput%d\n"),
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g.rc_4.control_in,
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g.rc_4.radio_out);
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APM_RC.OutputCh(CH_7, g.rc_4.radio_out);
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if(Serial.available() > 0){
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g.rc_4.set_reverse(0);
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return (0);
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}
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}
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}*/
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/*
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test the sonar
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